THE HIGH-FIELD GALVANOMAGNETIC PROPERTIES OF AuA12,AuGa2. and AuIn2 Thesis for the Degree of Ph. D. MICHIGAN STATE UNIVERSITY ‘ JOSEPH T. LONGO 1968 This is to certify that the thesis entitled THE HIGH-FIELD GALVANOMAGNETIC PROPERTIES OF AuAl AuGa and AuIn 2’ 2’ 2 presented by Joseph T. Longo has been accepted towards fulfillment of the requirements for Ph-D- degree in-_ 211323108 ////'/ /// / / ;/ _-- I v‘/ ____.—- “/Illajor professor Date Sept- 9: 1968 0-169 u; D- «4‘ - \ r.h ABSTRACT THE HIGH-FIELD GALVANOMAGNETIC PROPERTIES OF AuAl2, AuGag, and AuIn2 By Joseph T. Longo The Fermi surface topologies of AuX2 (X = A1, Ga, In) are investigated using high—field galvanomagnetic measure- ments. The high-field galvanomagnetic prOperties of the nearly-free-electron (NFE) model of the Fermi surface of Aux2 are also determined with the aid of the Harrison con- struction. The most important result is that the "open“ fourth zone electron sheet has hole orbits for_§ ll in AuAl and AuGa in disagreement with the NFE model. New 2 2 models are proposed for AuAl2 and AuGa2 which are in good agreement with experiment. Incomplete results for AuIn2 indicate that its Fermi surface may be similar to that of AuGag. THE HIGH-FIELD GALVANOMAGNETIC PROPERTIES OF AuA12, AuGa2, and AuIn2 By .,“I= Joseph T? Longo 3. A THESIS Submitted to Michigan State University in partial ful illment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Physics 1968 ACKNOWLEDGEMENTS I wish to thank Professor Peter A. Schroeder for his advice, assistance, and encouragement during the course of this research. I am indebted to Professors P. A. Schroeder and F. J. Blatt for the support necessary for the completion of this work. I am grateful to Professor D. J. Sellmyer of the Massachusetts Institute of Technology for the provision of his apparatus during runs at the Francis Bitter National Magnet Laboratory and for many informative discussions about interpretation of results. I sincerely appreciate the assistance I received from Andrew Davidson during these runs. I am indebted to my wife, Marge, and Dr. Gordon J. Edwards for their constructive criticism of the rough draft of this thesis. Financial support by the National Science Foundation is gratefully acknowledged. ii TABLE OF CONTENTS Page 1. Introduction 1 2. Theory of High-Field Galvanomagnetism in AuX2 9 Conductivity in High Magnetic Fields 10 Free Electrons-Closed Orbits 13 A Cylindrical Surface - Open Orbits 15 Open and Closed Orbits 16 A11 Closed Orbits 18 Real Fermi Surfaces 20 Description of the NFE Model of the Fermi 25 Surface of AuX 2 ‘I Calculation of Ap/p for AuX2 in the {100} plane 41 3. Growth and Preparation of Samples 52 4. Apparatus and Experimental Techniques 65 Analysis of Tipping Arrangement 69 Experimental Difficulties 72 Summary of High-Field Galvanomagnetic Properties 75 5. Experimental Results and Discussion 77 Hall Effect in Aux2 78 General Field Directions 78 Symmetry Directions 84 The High-Field Magnetoresistance of AuX2 9)4 The {100} Plane 9% Two-Dimensional Regions in AuAl2 and AuGa2 96 "Whiskers" in AuGa2 127 Models 136 Summary 140 6- Conclusions 142 iii List of References 144 Appendix A The Harrison Construction Program 147 Appendix B A Program to Calculate Ap/p in {100} for AuX2 158 iv U... I“ .~.c I... LIST OF TABLES Page I List of compounds 4 II List of semiconductors and metals (after 6 Sellmyer, ref. 3) III Dependence of Ap/p on the number of electrons 19 on open orbits IV Properties of the AuX2 compounds (after Jan 53 _e_§_a_l_., ref. 13) V RRR of AuX2 crystals 60 VI Impurities in Aux2 crystals 62 VII Samples selected for experiments 64 VIII Summary of High-Field Galvanomagnetic Properties 76 IX Hall data, general field directions 83 X Hall data, <1oo> and <111>; n = ne - nh ; An 88 XI Calculations based on a model with a Fermi sphere 91 fit to give experimental nlll values. NFE radius = 1.495, fit AuGa2 radius = 1.532, fit AuAl2 radius = 1.552. As usual 2wh/a = 1. There are hole orbits until 2 = .013 in the AuGa2 model and z = .062 in AuA12; see figure 9. Data in paren- theses is from early results of a study soon to be published by P. A. Schroeder, M. Springford, and J. T. Longo. XII Higher order open orbits for Fermi surfaces with 135 or <111>-directed primary open orbits. .0 I?» l. 2. \J'I 10. 11. LIST OF FIGURES A spherical Fermi surface A cylindrical Fermi surface Crystal structure of the AuX2 compounds. X is symbolized by the darkened Spheres. (After Jan .§§.al., ref. 13) Holes in the second zone of the NFE model of AuX2. (After Jan gt a1., ref. 13) Holes in the third zone of the NFE model of AuX2 in the reduced and repeated zone schemes. (After Jan gt a}., ref. 13) Section of the NFE surface in the flmuth zone. (After Jan g§.al., ref. 13) NFE surfaces in the fifth zone (left) and sixth zone (right). (After Jan_g§-al., ref. 13) Cross sections of the NFE surfaces in the third (clear) and fourth (shaded) zones at the pz values given for p || (100). Height of the unit cell = 200 0 Cross sections of the NFE surfaces in the third (Clear) and fourth (shaded) zones at the pz values given for E ||. Height of the unit cell = 1/(3)1/2.= .577 . Cross section of the fourth zone surface for § 290 from [100] in a (010) plane with orbits Open in [010]. Cross section of the fourth zone surface for_§ in vi Page 14 14 26 26 3O 33 33 33 12. 13. 14. 15. l6. 17. 18a. Page {110} with orbits open in . Cross section of third and fourth zone surfaces 33 for E in {111} with orbits open in . Cross section of fourth zone surface for_§ in 33 {210} with orbits open in (210). Cross section of the fourth zone with p at point 36 a in figure 18. Open orbits are separated by closed electron and hole orbits; net direction is 10° from in the {100} plane. Cross section of the fourth zone with g at point 36 b in figure 18. Open orbits are separated only by an occasional closed electron orbit; note how closed hole orbits have unfolded to form sections of open orbits or, in one case, pinched off the open orbit altogether; net direction is 180 from in the {100} plane. Cross section of the fourth zone with p at point 36 c in figure 18. Extended orbits on the fourth zone surface several degrees from the edge of the two—dimensional region. Cross sections of the NFE surfaces in the third 36 (clear) and fourth (shaded) zones at the pz values given for_§ parallel to (110). Magnetoresistance stereogram for the NFE model in 38 the fourth zone. b. Standard 100 stereogram l9. . Magnetoresistance stereogram for the NFE model in the third zone. Open and closed orbits on a "log-pile" surface with 43 the same topology as that of the fourth zone of the NFE model vii *1 -\ '\D 20. 21. 22. 23. 24. 25. 26a. 27. 28. 29. 30. 31. 32. 33. 34. variation of'a with angle for the "log-pile” model. Ap/p in {100} plane for log-pile model. RRR of AuGa2 crystals vs. excess Ga concentration. Phase diagram of Au-Ga. Schematic diagram of apparatus and circuitry. Experimental apparatus (after Sellmyer, ref. 28) Rotation and tipping geometry in the sample coor- dinate system. Magnetoresistance leads are con- nected at 1, 2; Hall leads at 3, 4, 5, 6. . Stereogram showing the effect in the sample coor- dinate system of rotating and tipping the sample in the magnetic field. Rotation and tipping geometry in the laboratory coordinate system. VH vs. B in AuAl2 supporting no open orbits. for general field directions VH vs. B in AuIn2 for singular field directions Simple model for the magnetic breakdown of orbits C4. Ap/p vs. V for all three compounds in {100}. B = 140 kG. Ap/p vs. V with m changed by .60 from figure 31. B = 140 kG. Ap/p vs. v in {ill} for AuAl2 at 83.1, 99.8, and 129.9 kG. The exponents computed from these graphs for B || (110) are m = 1.7 at 91.5 kG and m = 1.5 at 115 kG. Ap/p vs. v for A1<100> and G3 along paths indicated in the stereograms of figures 35 and 36. viii Page 48 7O 80 87 93 95 95 98 101 Page B = 145 kG. Magnetoresistance stereogram for Al. Bars 103 and dots indicate m>1.5; open circles mean m<.7 . Magnetoresistance stereogram for G3. 104 Magnetoresistance stereogram for the NFE model 105 in the fourth zone. Ap/p vs. v for G3{100} along path indicated in 108 figure 39 at fields of 130 and 145 kG. Magnetoresistance stereogram for G3{100}. 109 Ap/p vs. v for G3<110> along path indicated in 111 figure 42. Ap/p vs. B for_§ oriented along three crystallo- 113 graphic directions in G3. m = 0.0, 0.2, 1.8. Magnetoresistance stereogram for G3<110>. 115 Ao/p vs. W for A1<100> along paths indicated in 118 figure 44. B = 130 kG. Magnetoresistance stereogram for Al. 120 Ap/p vs. v for A1<111>. B = 130 kG. 122 Ap/p vs. I for A2(random). B = 130, 145 kG. 125 Ap/p vs. v for G3<110>. 126 Ap/p vs. v for G3<110>. 128 Magnetoresistance stereogram for G3<110>. 130 "Whiskers" and two-dimensional regions in AuGae. 132 Ap/p vs. v for G3<110> for six values of p. 133 Magnetoresistance stereograms comparing eXperimen- 138 tal open orbit regions (shaded) with the type of orbits (c = closed, 0 a open) determined on the models. ix 1. Introduction The determination of a metal's high-field galvano- magnetic properties has played an important and well docu- mented role in the understanding of its Fermi surface tOp- ology(1). Until recently(2’3’u’5’6) measurements have been performed only on very pure metallic elements at liquid helium temperatures so that a11_carriers perform many cyclo- tron orbits before being scattered. This high-field con- dition, mbg >> 1 for all carriers, is so rigorous that a metal crystal in a field of 20 k0 must typically have an impurity content of less than 10 parts per million to sat- isfy it. With the advent of zone refining techniquele), single crystals of non-transition elements meeting this re- quirement became available in the late 50's and were the object of extensive galvanomagnetic measurements. More recently, electron beam zone refining methods applied to the high melting point transition metals have been successful in increasing their relaxation time sufficiently to attain the high-field region in the laboratory(8’9) , though the rare earth and transuranic elements are still only available with 39's purity and escape investigation. , From the above discussion it follows immediately that the high-field condition cannot be satisfied in disordered alloys. Consider a .1‘5 concentration of element X in host element Y; this is a 39's element Y and requires the use of a megagauss magnetic field. More concentrated alloys than this have been studied by the de Haas-van Alphen (deA) effect and by the use of magnetothermal oscillations. These methods have the less restrictive requirement that ab? >> 1 for only a subset of all the carriers. This sub- set may be, e.g., the electron needles in zinc for which mc = .01 me(lo), thus increasing wk accordingly over its value for free electrons. Dilute alloys of up to 1% impurity concentration are, in fact, now being extensively investigated(11) because one eXpects large relative changes in small low effective mass pieces of the Fermi surface upon adding an impurity of valence different from that of the host. There is one class of metals, viz., metallic inter- metallic compounds, which could in principle satisfy the high field condition. Consider a compound AxBy in which x and y are integers and the A and B types of atoms each have a unique set of basis vectors in the unit cell. In such a compound, the potential would be perfectly periodic and the relaxation time, 7, would approach a as the temperature approached zero . Thorsen and Berlincourt were the first to observe the deA effect in a metallic compound, InBi, in 1961(12). Since then, Pearson and co-workers at the National Research 3 Council (NRC) in Ottawa, Canada, have observed deA oscil- lations in several binary metallic compounds and completed a study of AuAle, AuGae, and Auln2(13). The significant part of this research to someone envisioning a high field galvanomagnetic study of a metallic compound was that the residual resistance ratios, RRR = p(295°K) / o(4.2°K), of some of the samples approached 160. This is roughly equiv- alent to an impurity content of 60 parts per million (cf. page 59). In a field of 50 k0, one could expect that enough carriers would be in the high field region to give useful tOpological information. On this basis Sellmyer and Schroeder undertook a successful study of AuSn(2’3) in 1965. Later galvanomagnetic studies of metallic compounds included ZrB2(4), ordered Cu-Zn(5), and AuX2(6) (X = A1, Ga, In). Work is underway on AuSn(14) and Aqu2(15). Table I indicates the experimental progress to date. The face centered cubic fluorite compounds, Aux2 are of considerable interest, because changes in the electronic structure from one compound to the other should be explain- able in terms of the differing electronic cores at the X sites. An energy band calculation has not been carried out for these compounds, but one can Speculate on relative changes with the aid of the "Phillips cancellation "(16) theory If ltk> is the state vector of a conduction band electron, then Table I . Compound AuSn ZrB2 Cu-Zn AuAl2 AuGa2 AuIn2 Aqu2 List of Compounds. RRR(highest) 160 110 418 550 904 75 B(highest) 150 kG 12.7 RG 150 kG 150 kG 150 kG 150 kG 150 kG _publications 2, 3, 14 4 5 6 6 6 l5 5 p2 [an +‘VJ l¢k> = Eklek> where V is the periodic potential of the lattice. Orthog- onalize Itk> to the core states Ink) by letting ltk> = IXk> - EE_lnk> . Here le> is some smoothly varying function which is a solution of L§S+ v + VR] lxk> = EK lxk> where Vh is a non-local repulsive potential which can be shown to better cancel V as the core states become a more complete set of basis functions in which to expand lik>. If V + VR ~ 0, then ka> as eilc-T— unless E is near a Brillouin zone boundary at which the periodic V + VR mixes plane wave states to produce an energy gap. This is the basis of the nearly free electron (NFE) or one orthoganalized plane wave (1-OPW) Fermi surface model. Since the heavy elements have the largest number of core states, one expects that V +‘VR and therefore the energy gap should be a decreasing function of the row number of the periodic table. Table II, reproduced from Sellmyer's thesis(3), gives actual examples of this effect; the energy gaps separating the valence and conduction bands in semiconductors are listed. In a metal energy gaps at the Brillouin zone boundaries separate the conduction bands. These gaps should also decrease with increasing Z in a given column so that large Z elements should be more Table II. List of semiconductors and metals. (After Sellmyer, ref. 3) Position* Material Energy Gap_(eV)** Crystal Structure (2:4) C(diamond) 6 diamond (3.4) Si 1.12 diamond (4.4) Ge 0.75 diamond (5,4) Sn(grey) 0.08 diamond (5,4) Sn(white) metallic tetragonal (6,4) Pb metallic f.c.c. (3,5) InP 1.30 zincblende (4:5) InAS 0.33 zincblende (5,5) InSb 0.17 zincblende (6,5) InBi metallic tetragonal (3,”) M2231 0.77 fluorite (4.4) Mnge 0.55 fluorite (5,4) Megsn 0.25 fluorite (6,4) Mgng metallic fluorite * Position, (i,J), means 1th row, 3th column in periodic ' table. For compounds, (i,J) refers only to the position of the second listed element in the compound. ** Most of the energy gaps are taken from W. D. Lawson and ‘ S. Vielson,_Preparation of Single Crystals, (Butterworths Scientific Publications, London, 1958), pp. 241, 242. 7 NFE-like than the smaller Z elements. In the limit V + Vh = 0, a metal would become free—electron like (i.e. magnetic breakdown would occur with unit probability at every zone boundary). Several effects distort this simple picture. Relativistic corrections are important for elements with Z>55(17). Tin can be a metal or a semi- conductor depending on its crystal structure; thus structure changes in the columns of the periodic table present complications. Also, energy gaps due to Spin-orbit coupling increase with Z. Finally, if there is mixing of the high-energy core and conduction band states, this formalism falls by assumption; the noble and transition metals are in this category. Understandably then, excepI tions to the rule occur: Na is the most free electron like of the bee alkalis, but Be is less NFE-like than Mg. It is difficult to compare the elements Ca and mg because of differing crystal structures; the same is true of Al, Ga, and In. A comparison of the fluorite compounds, AuXépwould avoid this difficulty. Since the troublesome Au atom is common to all three, it may be that distortion from NFE behavior is primarily due to Au and secondly to the core states at the X sites. We conclude that AuAl should be 2 the least and AuIn2 the most NFE-like. The first experimental evidence bearing on this (13). The extremal hypothesis came from deA measurements cross section of necks in the third zone had the behavior predicted above; however, the "waist" areas suggested that 8 2 was the most NFE-like and AuIn2 the least. Results on the octahedron in the second zone showed the same AuAl deviation from prediction; the AuAl2 extremal areas were closer to the NFE values than those of AuIn2, while the existence of this surface in AuGa2 had not been decisively determined. The only comparison possible for the multiply connected surface in the fourth zone was the extremal area of the (100) directed necks. AuGa2 and AuAl2 both had values in close agreement with the NFE model. These results, published in the early stages of a magnetoresis- tance study of AuGa2, provided the incentive for this comparison of the Fermi surface topologies of all three compounds and the 1-OPW model through a determination of their galvanomagnetic properties. 5 I V 2. Theory of High-Field Galvanomagnetism in AuX2 Kohler realized in 1949 that high-field magnetoresis- tance and Hall effect data contain important information concerning the shape of the Fermi surfaces of metals (18); but the remarkable anisotrOpy to be found in magnetoresis- tance as a function of crystal orientation, discovered in 1938 (19), remained a mystery for 18 years. Lifshitz, Azbel, and Kaganov demonstrated in 1956 that, if all car- riers completed many cyclotron orbits before being scat— tered, the variation of the field dependence was indepen- dent of collision processes and determined solely by (20) geometric features of the Fermi surface. In 1964 Coleman, Funes, Plaskett, and Tapp (CFPT) performed the first calculation of the absolute value of the magnetoresistance in several symmetry planes for a simple open Fermi surface (21) Their using a single—relaxation—time approximation. work on the noble metals contained the assumption that the Fermi surface consisted of a Sphere pierced by narrow cylinders along (111) directions. They were successful because they applied a simplified geometrical theory to this geometrically simple model. The l-OPW or NFE model of a Fermi surface is geomet- rically simple to construct when done in the manner of (22), and prompted an attempt on our part to extend Harrison the single-relaxation-time treatment to cover the more com- plicated NFE surfaces. In the section, we develop the lO theory and calculate the magnetoresistance from a NFE-like model of AuX2. For readers suspicious of a constant-relaxation time treatment, we have included a table listing those galvano— magnetic properties which do not depend on this assumption in section four. Conductivity in High Magnetic Fields The Boltzmann transport equation describing the motion of a system of particles in phase Space is: V- T" at 0f +.:°vrf + p~v f = of ct p coll. (1) f is the statistical distribution function which Specifies the probability of finding a particle of the system with its position and momentum in the interval between_g and 3 + d3 in real space and between_p and p + dp in momentum Space. In an isothermal metal vrf may be safely set equal to zero; we wish to consider dc effects only so that of/at = 0. Finally we note that the scattering term must vanish in equilibrium when f = fo, the Fermi-Dirac distribution, and return the system to equilibrium when a deviation is intro- duced. The simplest possible form which satisfies these requirements is (Si-Lon. "' ’ 311:0”) 5*. NJ. 11 and the Boltzmann equation then reduces to T1 5 O (3) The equations of motion of an electron in a magnetic field are .2 = "let! X.§ : .X = vpc (4) In cartesian coordinates 15X = -IeIva I 15y = -IeIBvx pz = O , é = vpcgp = O if,§ (l 2. The electron moves on a curve of constant energy and constant pz which suggests a change to variables 6, pz, and a third variable u describing the motion tangent to the trajectory. We define du =_.___E- d t = \eIBdt. (5) I‘ VXZ —— Clearly, Q divided by a mass is a cyclotron frequency. In the presence of a small electric field in addition to the large magnetic field, we have '=. -=—ev-*' e vpe p l L_.2 l2 bz = -IeI§z (6) e =1912t = IeIB(1 “-5112 det Bv In terms of these variables, the Boltzmann equation is éof + p of + def = — f - f '5; zdpz '5; T(e)o ' (7) We seek solutions linear in the electric field (Ohm's law region) and thus set where_y is to be independent of.3, y =_y(e, pz, u)- Keeping only terms linear in_§, we have - e v-? of + e B e T:- SW of = —IeL;gy of l l—JEEO l l l l3 Sag-go 60 Note that this is equivalent to neglecting 3 in the equa— tions for pz and d. Since the electric field is arbitrary, + dV = d! 3 am = m =__l_ (9) The solution of this equation is L1 Jim) = Ute-mil ea”! 1(u‘)du' (10) -CD 13 Because - ‘ f A a8 a} ' e5“ du' = l , 1 is a weighted velocity average of_y along the orbit for.a distance of about l/a in the direction from which the elec— tron has come. The electric current density is I‘ '- =-2 1 Vde =0.” .9 .Jfifl. __ p .2 integrated over the Fermi surface inside each partially filled Brillouin zone. The approximation OfO/de = -6(e - u) dedpdpz will be excellent for low temperatures. Now de allows us to write 5 = 2e21 r _y.£ dpdpz. (11) (gm); ddB.Z. This eXpression can be readily evaluated for free electrons and for field directions perpendicular and parallel to the axis of a cylindrical Fermi surface. Free Electrons - Closed Orbits From figure 1, 14 P2 Px Figure l A Spherical Fermi surface l)z l3x Figure 2 A cylindrical Fermi surface 15 < II x vLcos(u'/m) , vy = vLSin (p'/m). Then €- II vLcosB.COS(u/m - B) from equation 10. Here 0 s 3 s v/2 and cot B = am. 8 is the Hall angle. Integrating, E V V du = mwvi-cosg.sins 13.2. y X 2 . ny — (nee T/Qm)COSB-Sln8 ne is the number of electrons in a primitive cell and Q is the cell's volume. The final result is cosea —cosg sing O ' 2 0 = (nee2T/Qm) cosg sins cos a 0 (12) 0 0 1 Note that a metal with equal numbers of free electrons and free holes has vanishing off diagonal elements since vy = 'YLSin(u'/m) for the holes. We will later prove this result for any carriers in the high field limit am < 1. A Cylindrical Surface - Open Orbits Consider the case of B 11 2 in figure 2. p o “A? on v5 .1 0:11 5., ..v. from equation 10. u 5° \ < \o 'o l\) u in m + 'o m '40 1 is the momentum length separating Bragg reflection planes. Then, u o 2 2 2 1/2 vidu=uV =:§(p -p) noeer 0’ = W e 2mm In a similar manner we obtain the other elements of the conductivity tensor. O O O o 2 .6 = nee T O 1 O (13) 29’” o o 1 Open and Closed Orbits A zero'th order model of an "open" Fermi surface might consist of allotting nfi "free holes” to a first zone closed surface, n: electrons to a second zone cylinder, and n: free electrons to a third zone closed sheet. The con- ductivity tensor for such a model is 17 c c 2 c c (ne+nh)cos B (nh-ne)cosBsins 0 3 = e21 (nc—nc)cosssin8 nO/2 + (nc+nc)cos23 O (14) e h e e h m0 0 c c o O ne+nh+ne/2 For experimental simplicity we measure the resistivity tensor in the high-field limit, a = v72. The transverse and longitudinal parts are: nO/2a2m2 (nfi-nc)/dm at m ec c c g r 2 o c c c c 2 (n -n )/dm n +n e T[ne/2(ne+nh)+(ne-nh) ] e h e h 0 = m 22 2 f c o 2 e TLne+nhrne/ ] and pyz vanish for this model. At 331 = 0 (3:0), C C O l/(ne+nh) O E = m 0 l/(no/2 +nc+nc) O ...._._. e e h e2 o c c T O O l/(ne/2 +ne+nh) The longitudinal magnetoresistance, (pzz(B)-pzz(0))/Ozz(0)a vanishes, but the transverse magnetoresistance does not: -A3 =[pxx(B)'pxx(O)l / pXX(O) P =(ng/2xngmgwwcn2 ,1 > O (n2/2Xn2+nfi) + (ng-nfil2 g... .»r . — au-u van .Pl nu $\3 ha .1, 18 Three possibilities are listed in Table III. The first case is realized in copper, silver, and gold with nC = 0. h CFPT's careful analysis of the noble metal topology showed that Ap/p = A§(wcr)2- l for B in a symmetry plane. A is a constant which includes the number of conduction electrons, approximately ng, and a measure of the cylinder area normal to B. d measures the effective width of the cylinder area parallel to_§ -- the other three (111) cylinders cause some of the orbits to close back upon themselves. Nevertheless our simple model should estimate the largest Ag. From CFPT one can easily calculate that the maximum n: = 1/5. Thus the maximum n: / 2n: = .125 which is in rough agreement with their largest A =.23. Cases II and III may be common occurences in metals with a large number of valence electrons per primitive cell, but the burden of calculation is now truly monumental since one cannot assume, in the manner of CFPT, that 0 (Open) 0 w IVY; xx _ 0 closed 0 closed) oxx(closed)0yy(open) xy( ) yx( All Closed Orbits c c DEM = pzz = nh-ne . wcT (16) c c and c c 2 EH =3” 2 nh+n€ (l7) er I... l9 Table III. Dependence of Ap/p on the number of electrons on open orbits. Case I Case II Case III no 0 c c 2 o fl§< <(ne' h)2 29. It (ne'nh) is > (n; nh)2 2 c c 2 c c 2 c c ne+nh ne+nh ne+nh 2 2 n°(nf_.j+ n°)(w I)? (wCI) (wot) - 1 .AA - ._§_ — l I p 2(n: — h)2 :- ,- v0- pry“ .- -4.- I ‘ C l . a I i“ -. “‘A rn 2O allow us to make estimates of n +nfi and ch from the experi- (D+O C c mentally measurable pxx, p , and nh-ne. xy’ pzz Real Fermi Surfaces For a more complicated Fermi surface we can simplify y for closed and open periodic orbits: - H I 1(11) = one ‘1qu loge “3(u')du' + I ea“ X(u')dI-I' } . (18) -cc 0 But 0 '14 t l ew'flu'mu' + 120 ea“ _Y(u')du‘ + ------ = '“o ' uo O a ' -d1 P O du' j e “_y(p0du' + e ‘03 e _g(p')du' t ........ , -uo ’“0 so that No Q , v( ) = ae’wf l I eau'v(p')dp,' +3 ea“ _v(u')du'(.(l9) _ H L d _. O eauo - l O “o is the period of the orbit. In the high-field region, we can expand_y in powers of a: 1(u) “,1(0) + av(l) + a 2v(2) + .......... (20) 1(0) =l-__ IHO X(Hl)dlll ,, (21) no 0 u 111(1) = 1 I140 u.'.Y(u')du' - 11.120 x(u‘)du' + "lo X(u')du' (22) u ‘7‘ 21 2 Ho , , Ho {“0 2 ,%__l .x(u )du -.u_) utx(u')du‘ +._1_I uky(u0du' “O O “O O ENOUO -U H - It) £(u')du' + l u'1(u')du' - (23) no do Only-139) is trivial; =.l_fuoz X (X X 2) du' = (g X AE)/UO (24) A2 is the momentum change from the beginning to the end of the period. Consider the case of all closed orbits. We use the .uo u .u notation < '> = I dpi and < '> = J du' . i = x or y. ”0 0 (o)- . W2 - (Vz >/uo Vél) = (u'vz'>/uo - “(vz'>/uo + u ll (0) _ W1 (Vi'>/uo - O Til) I I U (u'vi >/“o + 2 W: ) ‘ uW§l) + /2uo + (U'Vi'>u To determine 3 we must evaluate several integrals. Tue (0) _ 2 25 JO Vsz du — (Vz'> /uo ( ) (“0 ¢(1) I>< >/ + (V (V 1)“) v1 2 du = -u> = I 0 dp _de l0 x y x y .0 y lo x = -Area(e1ectrons) + Area(holes) (27) Ho (2) 2 ‘ £0 ViWi du = - /uo -“> + “> (28,29) . (“o (l) . The demonstration that J Vivi du = O is unnecessary: the O Onsager relations ok1(B) a olk(-B) predict that diagonal elements can only be even in a and reduce the number of in- dependent off-diagonal elements to three. For orbits open in Q, the only changes are W§O) = (Vy'>/“o = ‘Apx/“o ng) = (u'vy'>/uo - uApX/uo + u Then, 5:0 VZW§O)du = Apx/uo (30) (:0 vxv§0)du - 0 E20 vxv§1)du = -Apx/uo + u> (31) I'“° vinO’m = (nape/II, (32> 0 In the most general case, we cannot expect integrations over dpz to cause the vanishing of any of the functions of pz represented by these integrals. Thus the conductivity tensor has the form (I. 23 2 a coat aocCL aoc0L ' 2 0= 3. a. +8, + o 7: oca o oc0L ao aoc‘3L ’ (/3) a a + oca o aoc0L aoc a0 is a coefficient to be evaluated for open orbits only, aoc for both open and closed orbits. Inversion of this tensor gives us the experimentally measured resistivity tensor. Normally each piJ depends on all nine of the Okl’ but for the case of no open orbits a simplification occurs: = (-l)i+J cofactor(oij)/determinant(5) ; p13 Since determinant(5) = O( 2) = -c o o a 22 xy yx, ~B° 1 o ~B° / xy = ~ ~ 9 p l/Gyx B B , ( ) .qBO ’QBO .QBO Of the nine elements, only pxy and pyx do not saturate in the high-field region. These terms have a simple form since —- o = - 282Ig V [Ap(e) — Ap(h)! dpz (Eva); 3.2? _ n -n (35) BO 0 is the volume of the primitive cell, ne and nh are the number of occupied electron and hole states, respectively, v . nrv v so 3‘.- .V‘ 24 per primitive cell of the crystal. The prediction of ne-nh for any metal is given by setting the ”known” number of electrons in the conduction band equal to the number of states occupied in the various zones of momentum space, nV = 2F + ne+ (2J - nh) . (36) nV is the number of valence electrons per primitive cell in the crystal, F is the number of zones completely filled with electrons, 2J — n is the number of electrons in par— h tially filled zones with hole surfaces. Notice that, if nV is even, ne-nh may vanish. This actually occurs for all even-valence non-magnetic metals whose Fermi surfaces have been investigated and leads to a completely different re- sistivity tensor because the determinant(3) = 0(a4). These "compensated" metals are primarily characterized by elements Dxx’pyy = 0(B2) in contrast to the odd-valence'hncompensated” metals. For“singular” field directions(l) to be discussed in detail later, we must amend OXy: 0xy = -\el(ne-nh*An) (37) B0 An measures the number of carriers which have changed charac— ter on an open sheet. Thus a compensated metal can undergo ngeometric discompensation” along certain high symmetry axes 25 (<0001> in Mg and Zn), or an uncompensated metal could be- come compensated (this is almost the case for Cu, E || <111>). If there are open orbits on the Fermi surface, the determinant(5) does not simplify although it is still of order 32. The form of 3 is 32 B so a.» B Bo Bo (38) 0 B0 B0 Thus pxx goes as B2 with a coefficient dependent in a com— plicated way on the shape of the orbits since 0 G -O' 0' pxx = lyy zz zy_yz (39) U 0' -U U :10 +0 0 U L yy 22 zy yz xx yz xy zx +0 0 o a o o o o zy xz yx yy zx xz zz xy yx For certain symmetry directions, e.g. <211> and (110), it may be possible for a surface to support two bands of non- intersecting open orbits with different average directions. In this case all the elements of p saturate. Description of the NFE Model of the Fermi Surface of Aux2 Aux2 has the fluorite structure with the gold atoms lying on a face-centered cubic lattice and the X atoms occupying all the tetrahedral sites between the gold atoms (3 r\/’ /C) 4, Figure 3 Crystal structure of the AuX2 compounds. X is symbolized by the darkened spheres. (After Jan §§.al., ref. 13) Figure 4 Holes in the second zone of the NFE model of AuXe. (After Jan 2; al., ref. 13) 27 (figure 3). This structure belongs to the Space group ijm, so the Fermi surface will have full cubic symmetry. The NFE Fermi surface was first constructed by the NRC group(13) using the method of Harrison(22). A free electron Sphere whose volume equals the number of valence electrons times one-half the volume of each Brillouin zone is positioned about each body—centered cubic lattice point in momentum space. The occupied electronic states in the n'th zone are made up of all points located within n or more Spheres. We can thus construct the Fermi surface for each zone in the repeated zone scheme without considering the placement of the zone boundaries. For our model seven nearly free electrons are assumed and one-half the volume of each Brillouin zone is (1/2)(4)(2wh/a)3. The factor 1/2 arises because each zone can accommodate two electrons per primi- tive cell of the real lattice; we choose 2wh/a as a unit in momentum space to render the model independent of the lattice parameters which vary among the three compounds. To facilitate a study of this surface a computer program was written which performs the Harrison construc- tion calculations and plots the results with the aid of a 30" x-y plotter. A description of this program, which also plots Brillouin zone boundaries, is contained in Appendix A along with a program listing. The cross sections shown in figures 8-17 are from the computer plots. The first zone is full. The surface in the second zone has the shape of an octahedron holding about .05 holes Figure 5 Holes in the third zone of the NFE model of Aux2 in the reduced and repeated zone schemes. (After Jan gt al., ref. 13) 29 (figure 4). There is good experimental evidence concerning this surface in AuAl2 and AuIn2 from the deA experiment. The open surface in the third zone, containing .34 holes, makes contact with the hexagonal faces of the zone as do the noble metals (figure 5). deA data indicate that this contact area is reduced to about one-third of the NFE value in AuGa2 and AuIn and 1/15 of that value in AuAl this 2 2’ will considerably reduce the width of the open orbit layers, particularly in AuA12. The open electron sheet in the fourth zone (figure 6) has "arms" along the directions (100). deA evidence indicates that some of the AuAl2 extremal areas on this surface have values in good agree- ment with NFE predictions. It holds 1.14 electrons. The surfaces in the fifth and sixth zones contain .20 and .05 electrons, reSpectively (figure 7). Recently experimental evidence from deA confirms the existence of a surface in the fifth zone. (See reference in Table XI) The galvanomagnetic prOperties give no direct informa- tion on closed surfaces, but simply determine the number of full plus hole zones. A measurement of the Hall effect in AuX2 for general field directions supporting no Open orbits will give ne - nh; since closed and open surfaces contribute to ne and nh one suSpects that all the surfaces must be considered in computing this quantity for any model. For the NFE model of AuX2, ne-nh = = 1.0. A close examination of equation 36 reveals, however, .05 + .20 + 1.14 - .34 - .05 3O a———"———-‘-‘ , _- w... .——-—-——'——.— a- -- #— Figure 6 Section of the NFE surface in the fourth zone. (After Jan 23 al., ref. 13) Figure 7 NFE surfaces in the fifth zone (left) and sixth zone (right). (After Jan 5232 54., ref. 13) 31 that any model having seven valence electrons and a combina- tion of three full and hole zones also has ne - = 1.0. nh In addition to the general field directions, there are two singular field directions in the NFE model, <100) and (111). They are defined as axes Of higher than two-fold symmetry which are at the center Of a region Of aperiodic open orbits. At the singular direction the Open orbits intersect tO form closed orbits Of character Opposite to that Of the Open surface. Figures 8 and 9 are cross sec- tions Of the Fermi surface for g 11 (100) and (111) in the third and fourth zones. Clearly, there are closed hole orbits on the fourth zone electron sheet for g 11 (100) and there are closed electron orbits on the third zone hole surface for g 11 (111). To calculate n - n e h (100), we must subtract from ne those electrons which have for E 11 changed character, né , and add to nh the new holes, nfi. This is equivalent to subtracting the total volume occupied by né and nfi multiplied by 20/(2rh)3; this volume is A°d where A is the cross-sectional area Of a cell with A i; A(pz) and d is the pz width over which the orbits have changed character. An = né + nfi is to be added tO ne - nh for electrons on a hole sheet and subtracted from it for holes on an electron surface. Then B0 - a. u The calculated values give n111 = 1.035 electrons per prim- itive cell and n = 0.372 holes per primitive cell. 100 Figure 8 Figure 9 Figure Figure Figure Figure 10 ll 12 13 Cross sections of the NFE surfaces in the third (clear) and fourth (shaded) zones at the pz values given for_§ || (100). Height Of the unit cell = 2.0 Cross sections of the NFE surfaces in the third (clear) and fourth (shaded) zones at the pz values given for B (( (111). Height of the unit cell = (3)1/E/3 = .577 Cross section of fourth zone surface for E O 29 from [100] in a (010) plane with orbits open in [OlO]. Cross section of fourth zone surface for E in {110; with orbits open in . Cross section of third and fourth zone sur- faces for E in {111} with orbits open in <111>- Cross section of fourth zone surface for E in {210; with orbits open in 35 I gs I; (110) -) Fig. 9 34 These values differ significantly from the experimental values we will present later. We now turn to the investigation Of those field directions supporting Open orbits. From figure 6 it can be seen that as the field is tilted away from [100] in a (010) plane, orbits which are open in the direction [010] will occur for some values of pz on the fourth zone surface. A cross section for g 29° from [100] demonstrates this effect in figure 10. These periodically repeating orbits are called "primary" Open because they make repeated use of the same [010] arm of the Fermi surface when they cross the zone boundary. Secondary periodic Open orbits occur for some field directions in the (110) plane by repeated use Of [100] and [010] arms to give a [110]- directed Open orbit (figure 11). Fourth zone tertiary orbits Open in the directions (111) and (210) have also been investigated (figures 12 and 13). If.§ is applied in a direction close to the [100] axis in a non-symmetry plane (point a in figure 18), a plane perpendicular toug will intersect the Fermi surface to form alternating bands Of closed electron and hole orbits which are separated by two-dimensional aperiodic Open orbits as seen in figure 14. They are called two~dimensional since they are generated for a solid angle of field directions which is represented by an area on a stereogram, and they are called aperiodic since the direction cosines of1§ are incommensurable. As the angle between E and [100] Figure 14 Figure l5 Figure 16 Figure 17 35 Cross section of fourth zone with E at point a in figure 18. Open orbits separated by closed electron and hole orbits, net direction is 100 from in the {100} plane. Cross section of fourth zone with E at point b in figure 18. Open orbits separated only by an occasional closed electron orbit; note how closed hole orbits have unfolded to form sec- tions Of open orbits or in one case pinched off the Open orbit altogether; net direction is 18° from in the {100} plane. Cross section of fourth zone with g at point c in figure 18. Extended orbits on the fourth zone surface several degrees from the edge of the two-dimensional region. Cross sections Of the NFE surfaces in the third (clear) and fourth (shaded) zones at the pz values given for 3 parallel to . 37 increases, the number Of hole orbits gets progressively narrower and disappears; Observe figure 15 and point b in figure 18. If the field now angles towards (111), the number Of Open orbits begins tO decrease, and finally all the Open orbits coalesce tO form closed orbits "extended" over several zones; refer to figure 16 and point c in figure 18. If the field moves toward (110) from point b, the Open orbits persist even for a parallel to that axis. The cross sections for g 11 (110) shown in figure 1? reveal only closed electron orbits for small values Of pz, closed hole orbits for intermediate values, and Open orbits for the largest values Of pz. The presence of closed hole orbits for E 11 (110) requires that (110) be surrounded by a two-dimensional region Of Open orbits in order that the closed hole orbits may be "unfolded" by an Open orbit and then "refolded" into the electron orbits we observe for a general field direction. But the width, d, of the hole orbit layer cannot be determined on this model through the Hall voltage since the Open orbits change ox into a very y different form than it has in equation 40. For the field parallel to (211), there are non-intersecting orbits Open in directions (111) and (110), but there are no hole orbits on the electron sheet. All of these results are summarized in figure 18a which is a stereogram Of field directions. Shaded areas represent field directions giving rise tO orbits Open in a single direction and, therefore, to a B2 dependence of the magnetoresistance. 115 field directions E] Figure 18a Magnetoresistance stereogram for the NFE model in the fourth zone . ” Figure 18b Standard 103 stereogram. Figure 18c FagnetoresiSEance stereogram for the NFE model in the third zone. p V U I. PA in VV Cl. 0 a» ‘U. or AU 39 were sampled for open orbits by the computer. A similar analysis has been carried out on the third zone hole surface. (111) is singular but the layer of electron orbits on the hole sheet is so narrow that the extent Of the two-dimensional region is estimated at less than One degree. (100) is not singular. There is a two- dimensional region of Open orbits surrounding (110) due to the presence of a layer Of electron orbits when p is parallel to that direction. The complete results are summarized in figure 180. If the necks are diminished in size, we can expect a decrease in the size Of the two—dimensional regions and possibly the angular extent of the secondary periodic Open orbits, (100) and (110). The (111) primary open orbits will probably only be restricted in width parallel to B. Lifshitz and Peschanskii have analyzed several types of Fermi surfaces which were derived from an analytic expression for e(p). (23) For one surface which consisted of a three-dimensional grid of undulating cylinders whose axes are parallel to the directions , , and (111), the (111) and (110) two-dimensional regions overlapped. Inside this overlap, layers Of Open trajectories with different average directions are formed; thus the magneto- resistance must saturate destroying the connectivity Of the two—dimensional regions. These aperiodic open orbits must be intersecting rather than non—intersecting since all values Of pz will be sampled if repetition is not possible. . v F. s“ .u v ‘4 5-. :1. 40 Both our NFE results (figure 18) and our experimental data (figure 35) show that their analysis is not Of general validity. The reason for this is the artificiality Of a model with three sets of open "arms". Such a model cannot give non-intersecting orbits in two directions for B 11 (211) or (110), a known feature Of at least four Fermi (24,8) surfaces and our NFE model. Their model also cannot produce (100) directed orbits when H 11 (110), which occurs (25) for the copper Fermi surface and for our NFE model of Aux2 also. Thus we see that their model is of limited value. Two interesting variations Of their model dO occur on the NFE model Of Auxe. The most Obvious is the fact that the third zone has (111) directed arms while the fourth zone has (100) directed arms. The region Of over- lapping aperiodic Open orbits is centered entirely about (110). Our computer plots, however, indicate that the average direction Of Open orbits from both zones is the same. Secondly, the rather abrupt termination Of the two- dimensional region about (110) as §_moves away from (110) within the (110) - (111) - (211) Spherical triangle is caused by the intersection Of orbits Open in different average directions. One set Of orbits is derived from the (100) - directed orbits seen for g 11 (110); the other set arises from the unfolding Of the hole orbits for g 11 (110). For 5 not far from this axis these orbits "constructively interfere". But with g deviating by more than 10° from (110) they "close" each other Off. (I) (I? (3- Calculation Of Ap/p for Aux in the {100} Plane 2 We have developed a theory capable Of calculating the absolute value of the magnetoresistance for a complicated Fermi surface model with a single value of wa. We now wish to apply this theory to the NFE model Of Aux2 in order to predict the value Of the magnetoresistance. Unfortunately, this project is, in fact, a major undertaking and we resort approximating the Fermi surfaces Of zones 2,3,5, and 6 by Spheres and assuming the fourth zone necks have square cross- sections. The drastic nature of these approximations sug— gests that calculations on this model should be considered primarily as a guide to a more exact later calculation. However, a comparison between Oyy determined for the NFE model and this model was made and it indicates that the ap- proximation may be fairly good for a less than 300 from (100) (See figure 20). Consider figure 19. This "log-pile" surface has the same topology as the NFE Fermi surface Of AuX in the fourth 2 zone. For simplicity Of calculation, we have chosen the necks tO have a width Of 1/2 in units 2wh/a = 1. We con- sider orbits in the {100} plane only and note that there are six types, labelled A,B,C,D,E, and H. We must calculate , weighted velocity averages of these orbits and integrate over dpz to Obtain the various 013's. For our model each Open orbit is composed Of five 1 types of sections which we label in figure 19 as K, K. 1, 3 41 42 Figure 19 Open and closed orbits on a "log-pile” surface with the same topology as that Of the fourth zone Of the NFE model. 43 v i E Figure 19 B. p z ¢ p/z T= '/4o . 41 / dpl (A) = 8/2 p, L:””””§; I '/z 1+4 v, and v'. The closed electron and hole orbits are each com- posed Of only two types. From the figure, K = -dpt/vL = -(-3/4)/stinv = 3/4vs = m/2s. The Fermi velocity, VF = v, is given by nkF/m = 1.495/m m 3/2m. Similarly K' is m/2cosv = m/2c. Also v = m/3c and v' = m/3s. Since x changes with angle and pz, we leave it as l = I/v =(Xo2m1/3; X is the momentum length of x in the usual units 2wh/a = 1. The slow variation of.! with pz is rather troublesome; a considerable Simplification is Obtained if we average.! over the appro- priate range of pz for each type Of orbit. These values are I(A) = l/4c, 7(3) = l/4c, 7(0) = l/c, I(D) = 5/40 for the Open orbits. The ranges Of dpz are all s/2 if tanv, (vx >, (VX >, (uvx >, and “> all integrated over the appropriate range Of dpz. multiplication. the A orbits. By using I, this integration amounts to a simple We will now compute these quantities for = = 3c/2s — S/2c rK+)\ (uvx> = j deu + J K K+l+v = -v(l+v)l = —m/(802) u . u = F 0 d (vx > JO vX 0 IO = —V(VZV)vl = s/8c2 H = - = > v(vyv)vl VCK + 0'1 + (-vsv) + 0') + VCK PK+k+v+X u(-V)du f n .v 1‘ (U ‘i 46 Similarly, (uvxu> = -v212(x/3 + 0/2) = -l/72c3 = -(vx“>- The evalution of all the other quantities follows in a Similar manner. In order to take account Of the NFE surfaces in the second, third, fifth, and sixth zones, we have employed the following approximations: Oxx z 2Loxx(fourth zone) +(.39 + .25huJ 022:3 2[Ozz(fourth zone) +(.39 + .25)/mJ O z 2[Oxz(fourth zone)J xz Oxy = 2L0Xy(fourth zone) + .39 _ '25j (41) Oyz = 2Loyz(fourth zone)] Oyy = 2[ny(fourth zone)J The first three equations contain free electron approxim- tions for the .39 holes in the second and third zones and the -25 electrons in the fifth and sixth zones; we assume that the third zone necks are pinched Off. The factor 2 arises because there are two sets of each tYPe Of orbit in the fourth zone and because the momentum volume occupied by .39 holes, for example, is .78(2wh/a)3. (In the high-field region, the Hall angle = w/2 in equation 12). We drop the Th ‘A iv 47 factor 2e27/(27rh)3 for simplicity. The last three equations are exact in the high-field region. The results Of a computer program.written to carry out such calculations (Appendix B) are presented in the graphs Of figures 20 and 21. In figure 20 we have plotted the var- iation of 5 with angle in the {100} plane. We are using the convention 2wn/a = l, 2e2T/(27rh)5 = l, and a = 1. As a result terms of order a0, O O , appear in units yy’ yZ’ l/m; terms of order a, OXy and oxz’ are dimensionless, while d O an zz w o 2 o o T Uxx’ which is Of order a , 18 measured in units of m. o determi e n pxx’ 0 0 -0 0 pXX = __1yy zz zy yz , (39) _ + 0 0 0 (OnyZZ Uzycyz)oxx yx zy XZ _ O - O O O J + szoyzoxy Oszyy zx zz xy yx we first note that both factors in the numerator are given in units of (l/m)2 while all six factors in the denominator are given in units of l/m. It is obvious, then, from figure 20 that all terms containing O or OZX will be small so xz that - O pxx argyyozz Ozy yz . (42) - -O — O O O (nygzz Uzyoyz) .xx _zz xy yx The magnetoresistance can be calculated from pXX by noting that (Tu 48 O'yy \ . .. NFE fourth zone _. NFE third zone _ log — pile open Itotol open 1" e'o' I ’ \p (:00) (no) (me) (no) O'yz 0'" v y I/In' I/m: : aw ~I/m- 090“ -I- open '9otol a . n I | ('00) ". '°. (:10) (:00) W ("0) Figure 20 Variation of'E with angle for the log- 'p’u '-. total I/m‘ cIoeed (mm. a." 310' r: '4’ (no) O’xz closed (100) 'o ‘ o I In so (no) pile model. 49 2 2 - 331;: ' 2Wfi 3ma 1 =.m§3_° (wcT)2 (27W: )3 a3 2821’ We estimate 1 from the resistivity at B = 0 using a free electron approximation, p = maB/negw - n equals the number Of conduction electrons per cell Of volume a}. This number is 28, so that Ap/p = lAm-pxmeT)2 - 1 . (43) For some Of the samples measured in this work, wcvze 5, which gives Ap/p m 350m°pxx - l . (44) The results Of these calculations are given in figure 21. There are five distinct regions Of pxx depending on the number Of Open orbits. They are: 00-5O Case I behavior: a small layer of open orbits. 50-8O Case II behavior: a moderate number Of Open orbits whose importance is enhanced by the rapid decrease Of Oxy due to the thinning layer of hole orbits, H, and the thinning layer Of electron orbits, E; all terms in (42) are important. 80-13o Case III behavior: a thick layer Figure 21 Ap/p in {100} plane for log-pile model. 51 of Open orbits aided by the van— ishing Of OXy at 120 results in pxx.“ l/axx' 130-20O Case II and III behavior: a thicker layer Of Open orbits is moderated by a decreasing Oxx so that the first term in the denominator of (44) isgs constant. The second term is increasing, however, causing pxx to decrease. o o . ~ - 2O -45 Case III behavior. pxx ~ l/Oxx , Oxx is in turn dependent on fourth zone Open orbits for its variation. In addition to the complete calculation Of 0 for this model, we have determined Oyy from the third and fourth zone Open orbits of the NFE model. The results of that calcula— tion, also shown in figure 20, suggest that the log-pile model is a good approximation to the NFE fourth zone and that the Open orbits from these surfaces do dominate those of the third zone even without the known reduction in the size of its copper-like necks. The dip in the NFE fourth zone curve occuring over the range 300-45O warns us to look at pxx in this region with some suspicion since Uxx may also look somewhat differently in this interval. 52 3. Growth and Preparation Of Samples In this section we discuss the techniques used to grow , AuGa and AuIn . We also con- 2 2’ 2 sider the X-raying, sparkcutting, and mounting of the single crystals Of AuAl crystals. The general procedure for making the alloys was as follows. A small high-purity graphite crucible, usually with an alumina insert, was outgassed in a Lepel induction furnace, the temperature Of which was increased in several steps up tO l200°C in such a manner that the pressure remained at 10'“ mm Hg. The pure metals were etched if necessary, washed with distilled water, and rinsed with ethyl alcohol. The desired amount Of A1, Ga, or In (typically 2.5, 6, and 8 grams) was then placed in the crucible. Its weight was determined to .l milligram on a Mettler balance and the amount of gold necessary was computed and deposited in the crucible. The crucible was then placed in the induction furnace and heated to 100°C above the melting point of the compound (of. Table IV) either at a pressure of less than 10-4 mm Hg or in an argon atmosphere. Mixing was accomplished by agitating the melt mechanically and by the action Of the rf field. Several methods Of growth were attempted before high purity single crystals were produced. The first success was Obtained by vertical zone refining of AuGa with an rf 2 coil. The samples, prepared with the exact stoichiometry, had residual resistance ratios up tO 250 at the bottom of a; 5 .n‘ 53 Table IV. Properties Of the AuX2 compounds. (After Jan_§§ _gl., ref. 13) AuAl2 AuGa2 AuIn2 Resistivity at 2950K 8 13 8 (on-cm) Lattice parameter at 5.988 6.055 6.487 4.2°K (angstroms) Melting Point (00) 1060 492 544 54 the crystal. The graphite boat used was grooved so that the dimensions Of the crystals were 1/16" x 1/16" x 4". Three experimental runs on these crystals were disappoint- ing. At 55 kilogauss, the largest magnetoresistance Observed was 5 and no decision could be made on the state of compensation of AuGa2 since the field dependences were Bl'O-i .4 for all measured directions. The third crystal investigated, which had i approximately parallel to (111), did have a deep minimum with B ~v() (112) in its transverse magnetoresistance. Hall effect measurements were inconclu- sive: 1.2(ne-n (1.5 for several different general field h directions. For three reasons we decided to switch our concentra- tion to AuA12. Straumanis and ChOpra had determined that the extent Of the AuAl2 phase is 78.18 - 78.94 % weight Au<26). At the stoichiometric ratio there are .152 empty lattice Sites per unit cell in the Al sublattice and .076 empty lattice sites in the Au sublattice. But at the Al-rich border there was strong evidence that all of the A1 vacancies were filled. A crystal grown at the Al-rich border of the phase should be appreciably better than one Prepared at stoichiometry. The standard Bridgeman tech- nique was apparently not very successful when AuGa2 was prepared up to two atomic percent Off stoichiometry(27). Finally, AuGa has a rather high room temperature resis- 2 tivity Of 13 uO-cm, compared to AuAl2‘s 8 ufl-cm; this means 55 that oh? (free electron) for AuAl will be about 50% larger 2 than that for a AuGa crystal with the same residual resis- 2 tance ratio. Our first attempt to grow Al-rich AuAl2 in a graphite crucible was a failure. The crystal, which wet the crucible, had a residual resistance ratio of 33. We dis- covered that near 1000°c Al forms a carbide with the graphite; so we decided to place an alumina insert inside the graphite. The dimensions Of this insert were 1.5" long and .42" inside diameter. The bottom of this alumina crucible was bowl-shaped so there was some premature concern that it would be difficult to grow single crystals. The crucible and its contents were, as usual, sealed in a vycor tube filled with argon and lowered thru a three turn rf coil at a Speed of 1/2" per hour. The temperature of the graphite was measured with an Optical pyrometer and the rf current adjusted so that the hottest portion of the crucible was 60°C above the melting point Of AuAl Upon 2. breaking the vycor, we discovered that AuAl2 had wet the alumina; however, the alumina insert had cracked due to differential contraction upon cooling, and it was possible to pry Off the pieces of alumina clinging to the AuA12 slug. Back reflection X-ray photographs indicated that the crystal was single. The first two samples spark-cut from this slug had residual resistance ratios of 400 and 550 with J's parallel to (111) and (100) respectively. We designate these samples as A1 (111) and A1 (100); here A 56 refers to the compound, 1 to the slug, and the numbers in brackets to the current direction. Since studies similar to that of Straumanis and ChOpra had not been published for AuGa and AuInz, it was neces- 2 sary to determine experimentally the dependence Of their residual resistance ratios on the excess concentration Of one Of their constituents. Slugs of 0.0, 0.1, 0.2, 0.3, 0.4, and 0.5% weight excess Ga were prepared in the same manner as A1. The average residual resistance ratios Of crystals cut from these slugs were 190, 540, 680, 710, 660, and 200 respectively. The points in figure 22 representing individual samples show a considerable Spread about the average. It should be noted here that traces of Ga were found on the surface Of the slugs with 0.2 - 0.5% excess Ga. This may indicate that the phase exists to about 2% weight excess Ga; as a larger amount Of Ga is added it is energetically more favorable for the charge to reject this Ga, but at 0.5% the Ga phase begins to coexist with the AuGa2 phase inside the slug. See figure 23. A AuIn2 slug Of exact stoichiometry had a residual resistance ratio of 60. By varying the composition to both sides, the highest value achieved was 75 in a .1% In excess AuIn2 Slug. Several growth methods were tried in an attempt to improve on this value; these included vertical zone refining and horizontal zone refining and leveling. Crystals prepared in such a manner had residual resistance ratios less than 60. .soaooapsoocoo mu mmooxo .m> manomzao so: omvrw.‘3 passages 57 moos< no mam mm osswam so. so :2 so. so. :3 o. e. n. w. t i i i i i Ll r . ..000 IT . hr .rooo_ wooa< : m xqas 4‘ WEIGHT PER CENT GALLIUM IO L4 20 1.11 30 1 50 I 70 90 ill Kmo—J lo 800 "' 600 "" 400 — TEMPERATURE, l 200 '- é—- AuGa AuGa AuGa2 r T 60 ATOMIC PER CENT GALLIUM Figure 23 Phase diagram of Au-Ga. 59 Table V is puzzling for at least two reasons: AuIn2 cannot be prepared to within even a factor of ten as highly ordered as AuGa2, and AuA12 of exact stoichiometry can be grown with residual resistance ratios greater than 100 despite the fact that 1.9% of all the sites are empty according to Straumanis and Chopra. This latter effect is extremely peculiar because Sellmyer(3) has shown that AuSn qualitatively obeys the same empirical law as many of the elements, RRR ~r10u / I , l 5.1 $.10” (45) Here I is impurity or vacancy content in parts per million (p.p.m.). Thus 49's, 59's, and 69's metals typically have 1 3, and 10 . This is residual resistance ratios of 102, 10 reasonable because metals have room temperature resistivi- ties of l - lO uO-cm, while the resistivity due to impuri- ties or vacancies in dilute alloys is from 1 — 10 uO-cm. per atomic %. Assuming that AuAl obeys this law, a resin- 2 ual resistance ratio of 140 is equivalent to I = 71 p.p.m. or .007l%. This compares very unfavorably with the 1.9% from the Straumanis and Chopra study. The difference cannot be explained by the fact that compounds prepared with stoichiometric proportions may grow off stoichiometry; consider the limiting case of the Al-rich border: we expect I = .634% but, experimentally, I o'.0018%. A possi- ble explanation is that vacancies are segregated and not diSpersed throughout the material; adding extra Al or Ga 60 Table V. RRR of AuX2 crystals AuAl2 AuGa2 AuIn2 prepared prepared prepared exact Al-rich exact Ga—rich exact In—rich largest 140(13) 550 250 904 60 75 RRR 61 simply cuts down on the size and number of aggregates. The variation of residual resistance ratio over the slugs tends to support this belief. In this discussion we have neglected the residual resistivity due to the impurities in the Au, Al, Ga, and In. The ASARCO gold and indium had I ~'9 p.p.m. For the MRC aluminum, I ~'2 p.p.m., and for the ALCOA gallium, I «'1 p.p.m. Table VI shows that the residual resistance ratios of both AuAl2 and AuGa2 are appreciably affected by the impurity content of the starting material if the law RRR ~104 / I holds. For some combinations of impurity and host, a law in which 104 is replaced by 105 better fits the resistivity data; this is the case for mg in Cd and Sn in In. The numbers in parentheses are the appropriate changes which, in this case, clearly indicate order limiting of the residual resistance ratio. The use of 69's gold in these compounds could determine a suitable form of the law and possibly provide a most desirable increase in the average relaxation time. Samples were obtained by placing each slug in a small brass cup and securing with one metal and five nylon retaining screws. This cup was screwed into the face of a goniometer and the slug oriented to within 10 of the desired current axis with the standard Laue back reflection technique. The entire goniometer assembly was now mounted on a platform which was the high voltage side of a Servo Met Spark cutter. A stainless steel tube attached to the .‘..L “V: 0". —C Li: /-—- 5 a. vrl Table VI. Impurities in AuX2 AuAl2 prepared RRR 550 I from eqn. 45 l (p-p-m-) (180) I from starting 4.3 material (p.p.m.) I from ordering 13-7 (p p.m ) (175.7) RRR (if limited 2300 only by impurities) (23000) RRR (if limited 770 only by ordering) (570) 62 crystals. AuGa2 904 11 (110) 3.7 7.3 (106.3) 3720 (37200) 1360 (940) AuIn2 75 133 (1330) 124 (1321) 1110 (11100) 80 (75) 63 working arm at ground potential then cut out a cylindrical sample. Non-metallic debris was removed through a side arm Of the tube connected to a water pump. Since it is impossi- ble to obtain X-ray pictures from a Spark-cut surface of these compounds and etching is also of no benefit, the crystals were spark-planed on four sides to give a rectangular cross section. This is an extremely tedious process but well worth the effort when attempting to mount four orthogonal Hall probes. The final shape was roughly 10mm x 1.5mm x 1.5mm. Usually, major symmetry axes were perpendicular to each face. Mounting six potential and two current leads to a sample this size requires that it be firmly mounted to a large heat Sink. The Sites selected for probe placement were lightly abraded with a pointed object or a pencil sand blaster. This area was then tinned with solder until a very small bead was formed (less than .5 mm in diameter). The leads could then be quickly soldered to such sites. Wood's metal solder and Sta-Clean flux were used for AuGaé and AuIn . Rose's alloy was found superior for 2 AuA12. Table VII lists those samples selected for experiments. . .ukl ‘v‘ (3‘; 64 Table VII. Samples selected for experiments. Date Crystal RRR B(kG) Type of Data 8-65 G(randoml) 230 55 MR and Hall 3-66 G(random2) 205 55 HR and Hall 6-66 G 160 55 MR 9-66 Gl<1lO> 190 85 MR Gl<100> 200 140 MR G 160 140 MR C(randoml) 230 140 MR * Il<100> 60 140 MR * Al 550 140 MR * Al 400 140 MR 8-67 04(110 620 50 MR and Hall 04(111 775 50 MR and Hall 11-67 * 05(100} 475 150 MR and Hall * 03<100> 725 150 MR and Hall * 03<110> 904 150 MR and Hall * Al<100> 500 150 MR and Hall * A2(random) 550 150 MR and Hall * I2<110> 75 150 MR and Hall * Interpretation of data in section 5 is based on evidence from these samples. 65 4. Apparatus and Experimental Techniques The experiment consists of measurements of the magne- toresistance and Hall coefficient as a function of the mag- nitude and direction of the magnetic field. The apparatus used at Michigan State has already been described.(3) Since we will just present data taken at the 150 kG fields avail- able at the Francis Bitter National Magnet Laboratory, we will only consider the apparatus kindly provided for our use there by Dr. D. J. Sellmyer.(°°) Figure 24 is a schematic diagram of the apparatus and circuitry. The apparatus, shown in figure 25, permits the field to be oriented along any crystallographic direction for an arbitrary sample axis. This is accomplished by use of the worm gear which changes the tip angle m, and the spiral gear which changes v. The sample is mounted on an insert, I, which is removeable so that the crystal can be positioned by Laue back reflection techniques until a certain axis is parallel to BB'. The advantage of this positioning is that all rotations of t for any n will be straight lines on a stereogram centered at if_§ is in the plane {imp}. This is seen in figures 26 a and b. The drive rod D is con- nected at the top of the cryostat to a motor whose speed was normally adjusted to achieve a 180° rotation of v in 10 minutes. Rotation plots were recorded continuously on an X4Y recorder with the X axis signal coming from a linear ten-turn potentiometer coupled to drive rod D. We estimate 66 mthSOaHo was nonmamaam mo oapmsozom .zm oaswam _i _lHrI 1! II, — nooaoooa m1xfiHHH~ NIQN hmaomoz Om oaomsoO flu oaocoa oaocoaom J amppam .ox. oma . . 1; seesaw HHHA mama zoa, sopoauao>onmc —> , _ was assesses magnum unoaasO nmpmsoo Nowoa nohmmmom Omaaqad COpoonaam 67 I I711.» DRIVE R00 0 HI anNG " STAINLESS . STEEL TUBE RING RETAINING SCREW WORM DRNE l GEAR I SPIRAL SCREW- IN PIVOTS TWSEND an, \\a MACHWED \T‘ OFF TO CLEAR -, * wunwc ’/ TEFLON SPACER SPIRAL DRIVE GEAR Figure 25 Experimental apparatus (after Sellmyer, ref. 23) 68 .oaoam capo: laws on» Ca OHQEmm on» wcaaaap ocm wsHoSpoa Mo Seaman massaoaooo oaaEmm one CH poommo one waasonn EmawOOSOSm new oazwam 5,-9- : x ..o .m .s..n so needs ease mmea no oouoocgoo ops momma oonmpmamoaOpocwsz .EOszm Opocaoaooo oaaemm one CH zapoaomw mcaoaflp oco Coapduom mom ooswam A . a is NI \ (Ill 2 I«\ 69 that the maximum total error in our knowledge oflg with respect to the crystallographic axes is f2°. This estimate is based on accumulating the errors due to x-raying, Spark- cutting and gear backlash. If there are Sharp extrema in a rotation plot,the position is usually known to f.5°. Analysis of Tipping Arrangement Consider figure 27. In the xyz coordinate system, the current density is l O 0 008m 0 -Sinm J -l J = nyhJ" 0 cost —sinv O l O 0 O sinv cosy sinm O cosm O cosm O —sinm J o = -sinvsinm cosv -sinvcosm O costsinm sinw cochosm 0 COSm = -SinWSinm 0 J costsinm The double primed coordinate system is the sample‘s. We wish to measure voltages in the sample system. Thus, _E_H= R ER Let us begin by considering the case of all closed orbits. 70 IO ~< Figure 27 Rotation and tipping geometry in the laboratory coordinate System. aB° p aB° xy .. O O p = pyx aB aB aB° aB° aB° By straightforward matrix multiplication, aB° coseocosIIpXy sin‘IIpyx 5" = cosmcosirpyX aB° —SinmCOSIpyX sinvpXy —sianOSVpr aB° Therefore, E; aB° E; = cosmcoswpyx . JO . E; SinIpr By measuring E; and E; we can determine pyx’ 1 2 p = l EIVI2 + :EI‘IZI2 \/ (46) yx '—— .__, Jo cos2rpco:2 I + sin QII Careful analysis of figure 27 Shows that 2 2 cos°mcos°v + sin W = cos B . B is the angle of departure of the crystal from the x-y plane. Thus Now consider g to be || to x and allow orbits to be 72 open in a direction which makes an angle 7 with x and, of course,v/2 with B. One can easily show that 2 2 B COS 7 —B2cosysin7 B° - 2 p d -B cos7sin7 B°sin27 BO . (48) BO BO Bo If the crystal is now rotated by arbitrary angles m and I, we find that 2 E; a Ap/p a B (cosycosw + SiHYSinmSin¢)2. (49) Inspection of figure 27 gives us 2 2 Ap/o s B cos d . (50) d is the angle between the current and open orbit directions. 2 The B dependence due to open orbits is washed out if the open direction is about 900 from g. Note that this must always occur when B is near.§- Experimental Difficulties The ideal magnetoresistance behavior of B° or B2 is not usually achieved in practice because is not much greater than 1. Estimates of wcv give values of 3—10 at 150 k0 for three of the samples (Table IX). The wet of G3 is possibly greater than 10,while that of both AuIn2 crystals is less than 3. Copper samples with wchz 10 have a "quadratic” behavior of Bl'°’2’°. (‘9) The reason for the exponent not achieving 2.0 is simply explained. 73 Assume orbits Open in the x-direction; for simplicity, take 0 O - O 0 xx O O - O - ( yy 22 zy°yz) OXX Uzzoxyoyx If a = l/eBT is not much less than 1, _ 2 4 °xx T a axx + a bxx’ 2 0 = a + a b yy yy YY’ O = a + d°b zz 22 22’ O = d a + 02b xy Xy xy’ Oyz = ayz + d byz' Then, _ 2 pxx — al(wb7) + a2 (wa) + a3 + ..... The deviation from quadratic behavior depends on the value of wbv and factors containedhlthe aij and bij' Chambers(3°) has formulated an explanation of poor saturation if there are extended orbits for a certain direction of the field. For an electron which only traverses a section along one side of a closed orbit before colliding, the orbit appears to be Open. Thus in the field 2 region for which wclosed.7 >> 1 )> mext T, pxx‘¢ B , at fields such that wext'T )) l, pxx will saturate. Since we are only in the region wext'T ) 1, poor saturation is to be expected. (ext = extended) Values of the exponent, m, are calculated by sweeping the field to 150 kG at fixed angle or by performing two rotations at different fields, usually 130 and 145 kG. Unless otherwise noted m is the high-field exponent. 74 Because of experimental limitations, the procedure of reversing both current and field directions should be used in making measurements. We define VMR as that component of the voltage measured on contacts 1-2 in figure 26 which reverses sign with current but not with field. VH is defined as that part of the voltage on probes 3-5 or 4-6 which is odd in both current and field. It can be shown(3) that v [v(+1, +13) + V(+I, -B) -V(-I, +13) -v(-1, 43)] 1 MR 'E 1 V H - 17 [V(+I, +13) — V(+I, -B) -v(-1, +13) +V(—I, 43)] These current and field reversals eliminate thermal volt- ages from both'VMR and VH' They also eliminate magneto- resistive voltages from VH and Hall voltages from VMR caused by probe misalignment. Since the unwanted voltages appearing on the transverse probes can be as large as VH’ it is imperative that VH be measured in this manner. The unwanted voltages appearing on contacts 1-2 are usually small for field directions supporting Open orbits so that VMR = V12(+I, +H) to a very close approximation. For general field directions, however, V12(+I, +H) can be quite small («'5 uv) and errors can be appreciable. Unfortunately, the amount of magnetoresistance data required for a complete study of a metal far outweighs the necessary amount of Hall data. A compromise solution is in order: selected measure- ments on 1-2 are made in the rigorously correct manner to 75 estimate the magnitude of the discrepancies to be expected when only V12(+I, +H) is measured. From Eq. (48) one can see that the dominant voltage on the transverse probes will be prOportional to Becos a sin a when there are Open orbits. We have not studied these transverse - even voltages in any systematic way because the time-consuming field and current reversals must be employed in this case also. Voltage measurements were not appreciably affected by the noise level of .05 ~ .5 microvolts at the highest fields. With a two ampere sample current, Hall voltages were typically 10 u volts and resistive voltages from 5 to 500 u volts at 150 kG. Summary of High-Field Galvanomagnetic Properties The constant relaxation time treatment given in section 2 enabled us to calculate the magnitude of all the 01J as well as their field dependences. A summary of those high-field galvanomagnetic properties which do not depend on any assumptions about the relaxation time is given in Table VIII. These results of the Lifshitz theory are dependent only on the requirements that a semiclassical treatment is valid and that a certain field, Bo’ is exceeded. B0 is that field at which all carriers complete many cyclotron orbits before being scattered. 76 Table VIII Summary of High-Field Galvanomagnetic Properties Type of orbit and Magnetoresistance Hall Field * state of compensation . All closed and uncom- I~B° -QB pensated (neh nh) (ne-nh)le(coss . All closed and com- ~52 ~13 pensated (ne= nh) 2 2 *-)(- ~ ~ . Open in one direction B cos a B O -l . Open in two directions ~B ~B . Singular field direction '9B0 —03 (ne-nhIAn)|e\cosB * i.e. electric field per unit current density; 8 is the complement of the angle between g and B. **.Q makes an angle a with the Open orbit direction. 5. Experimental Results and Discussion Since measurements of the effective number Of carriers per primitive cell most clearly indicate deviations from NFE behavior in AuX2, we begin with a presentation of Hall data and a discussion of possible changes in the model. We follow this section with evidence from the magnetoresis- tance behavior of these compounds which corroborates our interpretation of the Hall data. High-field magnetoresistance is, potentially, a more useful phenomenon for investigating a Fermi surface than the Hall effect, but it is also more difficult for two reasons. The first is experimental: a large amount Of data is required to make a quantitative comparison with a model and, more importantly, data determining the angular extent of the two~dimensional regions must be taken at field directions which have carriers of unusually large cyclotron masses. Schoenberg has said that "the poor man's dHVA effect involves looking only at low mass pieces of the Fermi surface". In a Similar vein it might be said that the poor man's magnetoresistance experiment is concerned with measurements in high symmetry planes only. Secondly, if a good model of the surface is not available in an analytic form so that a computer can look for field direc— tions supporting open orbits, one must be both clever and diligent to make quantitative comparisons between theory and experiment. 77 Hall Effect in Aux2 General Field Directions From Table VIII and the discussion on page'71, we have E = ~ 0 B H ( II a ne - nh) e cos in the high field region at a general field direction supporting no open orbits. For the NFE model, Aux2 have seven conduction elections per primitive cell, one full zone, and two hole zones giving ne - nh = 1. Measurements of VH vs. B enable us to determine ne ~ nh and hence to check the above assumptions about the NFE model. The results for a AuA12 crystal with a residual resis- tance ratio of 550, (A2(random)), are shown in figure 28. Each curve represents a general field direction for which the magnetoresistance approaches B° dependence. For typical sample cross section (1.5 mm x 1.5 mm), current (2 amps), and at 150 kG, vH = - 8 u volts/(he - nh). we have shifted these curves vertically so that a line tangent to them at 150 kG passes through the origin; we can then simply use the value of VH(150 kG) to determine he - nh. Table IX lists the values of he - nh for AuAl2 and AuGa . The last three AuGa 2 2 a residual resistance ratio of 475, G3 {100}. The first values are for a crystal with value is for a crystal with a residual resistance ratio of 725, G3 (100). The exponent, m, of B in the magnetoresis- tance is also given. This eXponent is a better measure Of the attainment of the high-field region than the linearity 78 79 .mpfiogo Como o: wcflpaoamsm mcoapooafio UHOHM Hmaocow sow m H<3< CH m N>dv :0; as. c .\/ /~\ mm maswflm 80 _+u 2: 1.: .N+":cloc o .22 a55ml ad)- oo. . on. .51.: oxen. .6 >1 7 m... 81 Of the Hall curves. Generally, the higher m's correspond to larger deviations from he - hh = 1. Note that AuAl2 tends to have he - nh ( 1, while in AuGa2 he - nh is usually greater than 1. Any deviation of ne - nh from integral values indicates that some carriers are still not in the high-field region because of their low mobility (high cyclotron mass). The sign of the deviation indicates (1) whether such carriers are electrons or holes . Thus in AuAl2 electrons appear to be the lower mobility carriers while in AuGa2 the situation is reversed. The AuAl2 behavior is fairly easy to understand on the model. The Hall vast majority of the fourth zone closed electron orbits are extended over several zones. From plots Similar to figure 16, one can easily Show that the cyclotron masses of these orbits are several times the free electron mass. From the same plots, the cyclotron masses of the third zone hole orbits are calculated to be usually less than the free electron mass. Thus we predict that the number of electrons not in the high field region will be greater than the cor- rSSpOhding number of holes, ne - n ( 1. On the NFE model, h the AuGa Hall values are hard to understand. Since VH/IB 2 is known within 1%, the only other source of important experimental error is in the measurement of the sample dimensions. These were made with two micrometers; values were averaged for several attempts. We estimate the possible overall experimental error at less than 5%. There is only one group of field directions on the NFE model for 82 which the third zone extended orbits have cyclotron masses larger than those of the fourth zone. It is just outside the two-dimensional region of figure 19 and within the (110), (111), (211) Spherical triangle. The AuGa2 values were not determined here. Hall measurements can be combined with magnetoresis— tance measurements to give an estimate of ne + nh and (we?) (equns. 16 and 17). For G3 (100), 2 2 n + n n + n _.._ .4..... == (_IL...E) = h e 922 3.0 uv nh - he .98 nh + h6 = 1.22 x nh — _1 =7.8= + eCDT pxx h me? = 9-5 From the NFE model, nh + he .39 + 1-39 = 1-78- The experimental approximation is probably too small; from deA data(13), we estimate that he + nh ~'1.6. A free-electron (F.E.) calculation of mb(f), using the resistivity at 4.2°K, predicts a value of 4.5. The experimental wb's are cer~ tainly as large as mb(F.E.), and thus the (7) Obtained from D (4.2°K, 0 k0) seems to be an underestimate. Similar analyses of two other crystals have been carried out with the results also listed in Table IX. We conclude that for general field directions our data for AuAl and AuGa and 2 2 calculations based on it are in substantial agreement with the NFE model which predicts an effective carrier 83 Table IX. Hall data, general field directions. m ne-nh ne+nh wcT(calc.) wCT(exp.) F.E. 0.00 7.00 7.00 N.F.E. 0.00 1.00 1.78 G3 .20 .98 1.22 4.5 9.5 I G37100} .51 1.13 1.26 2.8 5.2 .42 1.25 1.49 2.8 4.4 .74 1.01 1.88 2.8 3.5 A2(random) .38 .81 1.32 4.6 6.5 89 1.15 2 90 4.6 3.0 .50 .99 1.70 4.6 5 l .25 .95 1.38 4.6 6.0 84 concentration of l electron/primitive cell. Due to time limitations, we did not attempt measurements on the rather impure AuIn for general field directions. 2 Symmetry Directions Four symmetry directions are Of interest to us; they are (211), (110), (111), and (100).(2°) With the field parallel to (211), Hall voltages in all three compounds were buried within .5 uv of peak-to-peak noise at 150 kG. A slight monotonic decrease with increasing field was noted. When this behavior is coupled with a saturating magnetore- sistance, as it is here, we can state with some certainty that there are non-intersecting orbits open in the two directions <110> and <111> (Case 4., Table VIII). This is in agreement with the NFE model: on the fourth zone surface there are orbits open in (111) and (110); in the third zone, there are orbits open in (111) only. The behavior for B 11 (110) is somewhat clearer now than it was in an earlier report(°), but by no means trans~ parent. The Hall voltage is linear in B with a slope which depends critically on alignment with minima associated with (110) in Ap/p vs. t curves. The magnetoresistance itself is a rapidly varying function near (110) with exponents ranging from .25 to 1.5 at the minima. We will later argue for Open orbits when B 11 (110) in agreement with the NFE model. The Hall behavior in all three compounds is con- sistent with the model also (Case 3, Table VIII). ./\ 85 Major discrepancies with the model occur when B is parallel to (111) and (100). Figure 29 displays the Hall voltages in AuIn2 for the NFE model. The eXperimental curves have been shifted vertically as in figure 28. The value of n100 = :68 means that there are .68 holes/per primitive cell compared to .372 on the NFE model. Electrons Oh the fourth zone sheet being replaced by holes must entirely account for this value if deA measurements Of the third zone necks are correct in predicting a smaller area so that no An arises from this hole surface. For B 11 (111) we see that V first swings positive and then H crosses back at 60 kG. Further, the curve has been dis- placed more than its total voltage drOp. The AD/p vs. B sweep here gives m = 1.08 at 150 kG. Thus the value n111 = +1.34 cannot be relied upon. The difficulty is caused by the low residual resistance ratio (75) of this sample. Table X contains all of the results including 111 for AuAl2 and AuGae. values for AuGa2 and AuAl2 are less than 1.0 reliable values Of n The h111 even with a 5% experimental error. We must conclude, then, that there are hole orbits on an electron sheet for this field direction in these compounds. Inspection of figure 9 reveals the sensible way for this to occur. If the NRC group<13> is correct in postulating that the fifth and sixth zone electron pockets have been emptied by the lattice potential, the remaining three zones must contain them. From figure 9 it is clear that the cut at p2: 0.0 86 Fiaure 2 ' ° C 9 VH VS. B in AuIn2 for Singular field directions. ‘ ....... 87. A 201“. VH (’LLV) ‘ I . ///’ "‘ .372 "l0“ e~\‘ I I 7 [’7 -\\‘\\ +l.34 9‘ “‘~\\\ AUInZ “~+|.035 _.-.10-- I-OPW -_ V := .158.- ,LLV CII I50 _20___ n = no."nh¥An 88 Table X. Hall data, and (111); n = ne-nhztm. m n100 m n111 F.E. 0.0 7.00 0.0 7.00 N.F.E. 0.0 -.372 0.0 1.035 I2<110> .57 —.68 1.08 (1.34) 03{100} .32 -.63 G3 0.0 -.62 .48 .89 03<100> .38 —.68 .50 .92 Al .43 —.79 .36 .57 89 produces electron orbits which are closer to contact than the orbits Of any other section. Thus an excess of electrons in this zone could produce the required hole orbits. There is a catch, however; the NRC group has tentatively assigned a dHyA frequency to these very electron orbits in AuAla, called 04 in figure 6. They point out that this frequency Should continuously join on to the frequency they have postulated for B4 as the field is swept towards <110> in the {110} plane. In fact, both frequencies are restricted to 5° intervals from these major symmetry axes. The reason for the restricted angular range near (111) appears obvious from our Hall data; their frequency corresponds to the area of the hole orbit, which will clearly vanish for some angle of deviation from (111). unfortunately, the sign of the effective mass of m*(Cu) is not known. Note that there are two types of hole orbits; the one centered at V is extremal while the other, centered at the corners of the hexagonal unit cell, is not. The easiest way to make quantitative checks of this postulate is to increase the radius of the Fermi Sphere until the desired n111 is reached and then calculate the area and angular extent of the orbit by running the Harrison construction program in the usual manner. We can only hope for an estimate with this method since the NFE fifth and sixth zone electrons are almost certainly prefer- entially located in the ravines hear the sharp tips of 04. This "corner rounding" occurs because in general the 90 periodic potential of the crystal lattice acts to reduce the exposed area of the Fermi surface.(1°) Thus the (100) arms probably are more cylinder-like than appears to be the case in figure 6. The results of the calculation are given in Table XI. The models which were fit to give the experimental n111 are in better agreement with deA and n100 results than the NFE model. The A4 results are noticeably bad but we expect this as a result of "corner- rounding". There is one possibility of salvaging the NFE model and that is to postulate magnetic breakdown of electron orbits like C4 to form the hole orbits Observed. Several experimental facts discredit this postulate. We would expect AuGa to be most easily broken down from the argu~ 2 ments in section 1, but our nloo and n111 values indicate the Opposite occurrence. A much simpler eXplanation is that AuGa is more nearly free-electron-like than AuAl 2 2 and that both breakdown fields are greater than 150 kG. If breakdown is occurring, we can set an upper limit on the field at which breakdown will be complete. In AuAl2 our Hall curves give values of 10111 = .57 and h100 = -.79 within 5% for B > 50 kG. For our best AuGa2 crystal, a 5% tolerance is maintained down to 25 k0, while for the poorest crystal, VH vs. B is linear to one part in 20 above 40 kG. We can demonstrate that breakdown is not complete at 25 - 50 k0 if we assume that a simple breakdown model has validity here. 91 .mmm.a n masons m.H mo.H). mm.)\ AO.HV m.H .sa 8. t... S... on. me. 1... mm. mo.d2 N.H2 Amo.av mH.H am 2 84:8 ”WNW om: omz. code Aooa . om). AHHHV no omens so u s.a m.a>. s.Hz_ s.a -osomwamawmm men.u ms.u :m.: 40.: ms.: ooas mno.H am. am. am. am. Haas moose maesa msosa Nessa moose wages mmz :maoooe pan: <>mo poommm Hamm .Owsoq .B .h was .oaommaaaam .2 qnooooanom .¢.m mp oosmaansa on Op zoom meson a mo mpazmoa sages Eon“ ma mononpsoama 2H when .m oaswam mom mmaasd SH moo. u a one Hooos mouse one as mac. n u shoes nosoao each one oases .H n s\eem Hoses as N m Haze one .mmm.a a masons mesa can .mms.a n assess maz .nosao> Haas amucoEHaomxo O>Hm Op paw oaonmm Sahom m Spa: Hooos s so oommn mCOHpmHSOHmo HN OHQSB 92 The probability of transition between two orbits coupled by magnetic breakdown is given by(°1) -B /B P = e ° where B = KA2 mc/e eh K m 1 o F ’ A is the gap separating two energy bands. Our data indi- cates that Bo <( 50 k0 or B0 >> 150 kG when the field is parallel to <111> or (100). Assume B0 = 10 k0 (250 kG) then with 6F = 9.4 ev, A ~'.l ev (.5 ev). Now we make a rough estimate of A and Bo from the dHVA results by noting from figure 9 that C4 must breakdown via C3 to give the experimentally observed area for the hole orbit. We con- struct a simplified two-dimensional model (figure 30) in which C4 is represented by an electron overlap into the second zone, and C by first zone holes. Then we have 3 1 5A In AuA12 m*(cu) = 1.5 me, the area of the NFE C4 = 1.7(2wh/a)2, and the measured area = l.4(2vh/a)°. Therefore ~ 2 107 - 10 L a. __ A2 21~(1.5 me} ’ '6 9V BO o: 360 kG Similarly, with m*(03) = .58 me, a measured C3 area of .6 (21rh/a)2 and a NFE area of .65 (2wh/a)2, we obtain A = .26 ev , BO «'68 kG 1 93 .\\\\\\\\ 94 Evidence that this estimated breakdown field of 68kG is too low is given by the normal behavior of the magneto- resistance vs. B curve which does not have the predicted anomaly at a field:~ Bo/2 .(32) We conclude that our Hall measurements along (100) and (111) give strong support to a fourth zone electron sheet which has hole orbits for B (1 caused by the contact of orbits 04' The High-Field Magnetoresistance of AuX2 The {100} Plane Figure 31 displays the magnetoresistance of all three compounds in the {100} plane. Calculations of wcT for Al and G3{lOO} give values near 5 (Table IX) so that the curves for these compounds can be compared directly to the calculated curve of figure 21. The agreement is good considering the assumptions about the relaxation time and the shapes of the surfaces that went into the calculation. Actually, the AuGa2 curve should be multiplied by the factor l/cosga = 1.16 because.§ is 22° from in G3{1oo}. This improves the fit slightly. The fact that there is no dip in o the experimental curves at v a218 suggests that hole orbits persist on the real fourth zone surface for several degrees beIYond the 18° range on the log-pile model. Figure 20 shows 11 then be why: oxy(closed), axx(closed), and O’xx(t0’cal) W1 larger at 18°, while (oxy(total)| will be smaller. Hence A N.” I IZO‘ I l Goo)" 6 -.;_.;r -- 4 -- 2 r; .- 000) "r. "°° (no) Figure 31 Ao/p vs. v for all three com-‘ r no; pounds in klcc) B = 140 kG 95 AP/P I IZO' ~ and . The axis is singular. The magnetoresistance at (110) was determined to be "quadratic”, m = 1.5 at 115 kG, by rotational measure- ments on Al at three different fields. See figure 33. The very large magnetoresistance observed in figure 31 in- dicates that Ap/p is probably quadratic at (110) in AuGa2 also. We attribute the sharp drop in magnetoresistance near 0 in figure 32 to the cosga term of Table VIII, a = 90 . Figure 35 provides an illustration of this effect. Two-Dimensional Regions in AuAl2 and AuGa2 The region between 15° and 30° in figure 32 is begin- 97 Figure 33 Ap/p vs. 4; in {111}- for AuAl2 at 83.1, 99.8. and 129.9 kG. The eXponents computed from these graphs for B (l are m = 1.7 at 91.5 kG and m = 1.5 at 115 kG. A P/P ‘40-- 20-- 98 l I . l AuAl2 Befinbu} " 13° I o <2”) (“0) ' Figure 33 (an) I -HV..--—.hofll i--‘.. -_, .-. .. _\.’.“~-_~..._~w . —--- a” s. .— .~...-.'.--m _-.. ~—~—v~n.-AI-‘ "-2 ., 99 ning to saturate because the orbits here are most likely not open but extended. By tipping n to several angles and per- forming rotations at two different fields, a systematic ex- ploration of field directions supporting open orbits can be carried out. We begin with a presentation of the results of such an analysis on Al and G3. We will also fol- low this with a discussion of our results on several other crystals. Figure 34 displays the magnetoresistance of Al and G3 along the paths indicated in the stereograms of figures 35 and 36. In the latter figures we use the symbol of an open circle to represent "saturation", i.e., Ap/p =Bm, m (.7; and we use a solid line or dot to represent the extent of "quadratic" field dependence, m >l.5. Intermed- iate or unknown values of m are not marked. Shaded areas of all stereograms represent probable regions of open orbits primarily as determined by data on one crystal. If infor- mation on a certain section of a stereogram is not available from this data, we have supplied this information from re- sults on other crystals. The similarity of the two curves of figure 34 is as remarkable as their disagreement with the NFE model which predicts a B2 dependence along the entire rotation path. A summary of the results of several similar rotations is given in figures 35 and 36. The behavior pre— dicted by the NFE model in the fourth zone (figure37) is not seen experimentally. Open orbits from the third zone of the NFE model could give a qualitative explanation of the 100 Figure 34 Ap/p vs. W for Al and G3 along paths indicated in the stereograms of figures 35 and 36. B = 145 kG. 101 1 l L L l A WP 200— (,6 = 63° . AuGa, -2oo leo— ' -l60 ‘ 120'- eo-a (J (.__ Figure 3” 102 opmoapcfi mpop one whom . N. v E cmoe mmHohHo Como mm.a A E .AooHvad pom Emswomsopm mosmumammLOpocwmz mm ohswflm 103 'Dl woos ~23 mm cpswam 101+ .AOOavmc you Edhmoohopm cosdpmamomOposwmz mm onsmam [it'll]: .Ilnllcl‘llll 105 .- .ccon sphsom ca Hopes mmz you smnwomscpm.consumamoHOposwmz hm onswfim 1" .‘Il’nl I .Itlnc I mcoN £50m . , mmz .‘ ‘50.! tit .1 0 106 (110) two-dimensional region in AuGa2. However the re- striction of the neck size observed in deA almost certainly eliminates this possibility: calculations of the extent of this region with a Fermi radius increased.§.5 per cent to give the deA area of the third zone neck show that open orbits exist only within 10° of in AuGa2 and 5° in AuA12. We have a considerable amount of supplementary data on AuGa2. Figure 38 is the result of a rotation of G3{100} along an arc of the great circle indicated in figure 39. Seven other rotations yielded the remaining data on this cry- stal with the results symbolized in figure 39. Note that m assumes more intermediate values here than it did for G3, a better crystal. The saturation observed inside the sug- gested two—dimensional region results from the cosga = O are being shifted from the {110} plane since_§ is 220 from (100). Our best data relevant to the directions of.§ suppor- ting open orbits in AuGa2 comes from G3<110>. We observed extremely sharp structure in rotations, e.g., figure 40 and only a minority of the measurements of m gave equivocal results. (See figure 41) The analysis of nine pairs of Ap/p vs. V curves at fields of 125.0 and 14”.? kG resulted in figure 42. Most of the dots represent higher-order open orbits which are "excited” as the field crosses low symmetry planes. A complete analysis of the extent of these "whiskers" from the major symmetry directions has been carried out 107 \ I Figure 38 Ap/p vs. v for G3£lOOJ along path indicated in figure 39 at fields of 130 and 140 kG. . Ap/P 4o- 20" <—— Le 1.6 (_— »<%- l.| <%- l.2 <—- l§335 c “? (- 1.55 Figure 38 109 oono I soos< 110 .m: omsmag CH Umpmoapcfi good mcoam Aoaavmm mom a .m> a\a< o: omswflm o: madmam h‘l” ; 1 101. 10.10.. |I . _ 1 1-“.1.-. - .1. * 1.. . . _ 111 1 I‘ll!!! I." 1! 1-.l 01'- . 1.: ..- 1 .lv ...._..&'L.-t-$ L'l "’ —-.—... “.1,— -— .— .IOO. . _ . . f _z 71 . m . ’0 _ 1 -11 1. ‘ .1111----.--1-1..-_-: .5}- Islon. a . _ .. . _ 111....11... 1 1 ..fi...1£11.. .1 .1 1. 1 ........ 1o -1 1 1 1. 1 w131.wt 3:.“ .._ H . _ . O. _ H” . . .a * H :- .../.. T. ,6 ...._ _ .oE . e Aozv :2... noos< ! . . ”1-1.1: T o: fi¢¢.um aqua. __._ _ a _ m _ _ _ __ 11-1-...1..1-- 1111.41-11 1.a.....111_.1-1-...1 1 com . _ _ M p _ . _ . 1 1 11.1111 1. ..1-.-.-11..-.1+:.1 11- 11 .. _ . _ p r0 . flu”! 112 . m.H «m.o «0.0 u E .Aooavmm CH mcoapoosfio canamsmogmumsfio ooscp mcoam popcmfiso m .Hom m .m> 934 a: ossmam 113 35m A _ on. 00. on Aoo_v :m 20:09.5 Bo: Benson 5 m r0. A00; 5 .m. 1cm soos and Al with the (110) axis parallel to BB‘ of figure 25. We cannot make any definitive statements about 32 regions of the stereogram from this data but experience has shown that, usually, saturation is associated with low, slowly varying parts of the curves and quadratic behavior with sharp peaks and the highest parts of the curves. Thus we can interpret these curves in a qualitative fashion. Consider figure 43. In the upper trace, we speculate that Ap/p is quadratic from 35° to 650 except at the minima where m takes on an intermediate value. From the lower curve, we guess that the two-dimensional region about (111) extends out approximately 10°, while the region about <110> measures 150 when the field is in the plane {211}. Figure 44 shows that these predictions, which were made before the 1967 runs, generally conform with the established results taken from figure 35. Figure 45 is a rotation of A1<111> along the same path as the upper curve of figure 43 to within 2°. The difference in the shape of the two curves is explained by the term cos2a. The peak at 180 in figure 45 is missing in figure 43 because the angle between the open orbit direction [010] and the current direction [100] is 90°. A similar analysis explains the difference in the relative height of other B2 “”3. 117 Figure 4 3 Ap/p vs. v for A1<100> along paths indicated in figure 44. B = 130 kG W 118 ' 30° ' so' A114, 40- 20- \\— 3 4o- cl) = 66.2° 111111112 - Ai (mo) 95 = 31.5° <1 1 11> \F A\ (In) Figure 43 (no) 119 .mn «Aswan Eopm meHELopop who; macawos Hmcofimcosfio1osp wcfipofigop mmosm pmpmnm .AooHvad mom EmsmooAmpm consumammnopocmwz :: ohsmflm 120 "3| :: madmam ouécae 121 Figure 45 Ap/p vs. 1 for A1<111>. B ‘ — 130 kG. L443. w 122 . 1 J '1 'AP/p AuAIZ- Ai (Ill) .. ' 4 4) = 18.9° 40- ac— 1 ‘ l 0. 30° Figure 45 60 123 regions. In all of the experimental stereograms, we have shown unexplained B2 regions near the axis (211). Some of these are close to, or in, the planes I210} and{2ll} and could be attributed to one-dimensional regions of open orbits. Others are not in high symmetry planes and evade explanation unless there is a two-dimensional region of Open orbits surrounding (211). (211) is not surrounded by aperiodic open orbits on the NFE model. Our data indicates that the (100) and <110> two- dimensional regions are not connected along {100} unless this region is very narrow, i.e., less than .60 (see figure 32 and the discussion concerning it on page 96). Our data indicates that the (110) and (111) Open orbit regions are probably connected in AuAl2 but not in AuGaz. However, there are some minor discrepancies. Figure 46 is a rotation of A2 (random) in which 3 is known to be 2 2 degrees out- side of 11101 at the heads of the arrows depicting the region of quadratic behavior. The upper limit of 40 on the connecting area is in disagreement with figures 43 and 45. Here we must appeal to the questionability of our inter- pretation of those figures and to the fact that there could be a 2° error in the knowledge of the field in figures 43 and 45 also. Figure 47 is a rotation of G3<110> very close to the {110} plane. At 12° and 63° we know that §.is 2° 1° from {110}. The rather large magnetoresistance seen here (values of m are unknown) suggests that the orbits are open .10. "I Figure 46 124 Ap/p vs. v for A2(random). B 130, 145 kG. 125 I 1 1 l [3,040 ‘ . , . AuAI2 - A2 (random) ‘ . _B_~ in {no} 160- f 120-?- 80- - 4 1 40- . 1 4 42° > 1 “"1 I ' 1 0° r3010) Figure 46 90° 126 1 _1 ‘1 l i AuGa A e ~ 2 WP . 2; '1 . J~Il (no) I soo— - — .. s=144.7 1c 1 N ,... 1 ._ "~— -—“.---_‘.— -‘~ - ‘ ' ZCHD '- 1 I I 1 1 1 __1.-.__.... 1 1 1 v" v.“ — .1...— ..~.. .—_.o . .-.I - ~— °( “5’ 3'o° I 4‘5" 8 1 6'0" 0 ~ ' {loo} ~ Figure 4? Ap/o vs. v for G3<110>. 127 in disagreement with our other results. The fact that these points are minima, however, leaves open the possibility that these orbits are merely extended. “Whiskers” in AuGa2 The sharpness of the {100} peak in figure 47 indicates that carriers on directed open orbits in G3<110> are rather far into the highefield region. (33) Using this cry— stal, which has the highest residual resistance ratio of any intermetallic compound on which data has been published, we easily resolved sixth and higher order open orbits in the magnetoresistance. The peaks on the left side of figure 48 are due to orbits open in directions , <210>, <310>, (511), (100), (611), (511), (311), (211), (533), (322), (111), <553>, <774>, (221), <331>. The two-dimensional regions of open orbits which produce the broad peaks are centered on (111) and (110). Note again the sharpness of the peak ob— served when p crosses {100} at about v = 130°. Several similar rotations with m varying between 60° and 90° pro- duced figures 49 and 50. The lengths of the whiskers in these figures are determined by noting the disappearance of a peak as m is changed. We demonstrate this in figure 51. At m = 72.10 we are inside the (100) two—dimensional region until v = 43°; the magnetoresistance is slowly varying be- cause only the coefficient of B2 is changing. When m is changed to 75.3°, we skirt the edge of the two—dimensional region. For g in certain symmetry planes only, open orbits 128 s , .on_ 9. be: .m 65 :2... .Aoaavmo toe s .n> a\aa ms ossmag com com com On 00. On. CON «\md 129 .AQHHVMU pom Esswompopm consumflmogoposwmz m: osswfim 130 w ._ .-..".r-..—~ - - - --—OH .— .- 1.. . m: madman 131 Figure 50 lWhiskers" and two-dimensional regions in AuGae. Figure 50 133 o .. 5w . . a so wosae> saw toe Aofiavme sou s n> a\ao am as an 9. 00¢ 00.? 90.? . 90¢ 09? 00V 00.? 00m 9 p Z 5 M. a M. I , he H :8 m m a w mm “Hm m 1100. -100. .o.om_ hem .56 .03 .05 2.3.1.. 2. MfumvnAN .émmw 134 still exist; the magnetoresistance acquires structure be— cause of the transition between saturating and quadratic behavior. At T = 81.7° the "fuzz" due to very high order open orbits has disappeared. Finally, at m = 90°, the 210 whisker has ended and the peak due to the crossing of the {110} plane has merged into a B2 background near <211> on the stereogram. The assignment of the 774 and 553 whiskers in figure 50 must be considered tentative since the planes {332} and {443} are within 1° of the position of.§ on the stereogram where the magnetoresistance peaks occur. However, the data is sharp enough that we estimate a maximum error of i .50 in v, which gives considerable weight to our assignment. Table XII gives the order of the open orbits arising from and (100) - directed necks according to the simple scheme used in section 2. (34) In copper the "whiskers" have a strength and extent that decreases with increasing order of the orbit. (25) From Table XII and figure 50, we see that if this property held for a complica- ted surface like that of the fourth zone of Aux2, the whiskers extending out of the (110) axis must be partially derived from the third zone surface with its —directed necks. We have already shown, however, that in the NFE model of the fourth zone the (111) open orbits exist for _§ anywhere in {111} while the lower order (110) open orbits vanish for p near (111) in (110}. Thus the lengths of the whiskers in AuGa2 may be explicable without appealing to 135 Table XII Higher order open orbits for Fermi surfaces with (100) or -directed primary open orbits. Order Possible open orbit directions 1. 2 , (110) 3 , <210> <3ll>, (331) 4 <211>, <310> <210>, <211>, <221> 5 <311>, <221>, (511), (531), <551>, <4lO>, <320> (533), <553> 6 <4ll>, <321>, <310>, <320>, <32l>, <510> <322>, <332> 136 third zone open orbits. Models A comparison of any of the experimental stereograms in this section with the NFE stereograms of figures 18 and 37 shows that the NFE model does not explain our experi— mental results on the extent of two-dimensional regions about (100) and (110). With a smaller third zone neck, it does not even predict the existence of one about . Another point of disagreement concerns the extent of Open orbits in the {110} plane. In all three compounds the magnetoresistance in {110} is quadratic unless the field is close to (211). On the NFE model {110} is not a one— dimensional region of open orbits near . As we pointed out at the beginning of this section, we must have an analytic model to obtain results we can compare in a quantitative way with experiment. The obvious choice is NFE models with radii swollen to give the n111 values since these models were successful in interpreting the Hall data at and various deA areas. If the Hall effect and magnetoresistance data are consistent, these models should also yield two—dimensional regions of approximately correct dimensions. Because of the cost involved C~ twenty-five dol- lars per angle), we limited ourselves to four symmetry and ten non-symmetry directions of.§ for each model. On the NFE model only one of the non-symmetry directions of'g gives the experimental result. 137 In figures 52a,b we summarize the analysis of general field directions and compare it with experimental results. Agreement is excellent for the AuAl2 model: all ten field directions produce the type of orbit eXperiment found. In the AuGa2 model four of the field directions give erroneous results and indicate that the two—dimensional region is too large while that about is too small. The AuAl2 model actually gives a better fit to the AuGa2 experimental results than the AuGa2 model for the ten non-symmetry direc- tions. The fact that the experimental two—dimensional re- gion near in AuGa2 does not extend a few degrees be- yond the range observed in AuAl2 is somewhat surprising since the experimental Hall coefficient at (100), as well as that obtained from the models, indicates that there are fewer holes on the electron sheet in AuGa2 than there are in AuA12( Table XI). This is a minor but interesting point for which we have no explanation. The behavior of the AuGa2 model near and (110) is in better agreement with ex- perimental data. Although the two dimensional region about (111) is too small, we must remember that the hole orbit layer is very thin on the model (less than five per cent of the height of the unit cell) and the tendency for electrons in excess of the NFE number is to deviate from rigid-band placement, resulting in cornerbrounding. Thus, it would seem that a small change in the model near the hole orbit layer could produce the experimental angular extent of the aperiodic cpen orbits near . Of great importance is the “—.. ‘-- A..~u .— igure 52 Magnetoresistance stereograms Acomparing experimental open orbit regions (shaded) with the type of orbits (c=closed, o=open) determined on the models. 139 fact that the two-dimensional region about on the AuAl2 model is clearly larger than the region about this axis on the AuGa2 model and furthermore that there is evidence that the (111) and (110) two-dimensional regions on the AuAl2 model are connected, while on the AuGa model they are not. These fea- 2 tures are in agreement with experiment. Thus, with the field near , our magnetoresistance data corroborates our inter— pretation of the Hall data, i.e., that the Open surfaces of AuGa may be more NFE-like than those Of AuAl 20 We find that there are extended closed hole orbits for 2 general field directions on these models. This is in disa- greement with our Hall data since ne-nh = 0 then. We take this as evidence that excess electrons do deviate from rigid~ band placement. The behavior Of the models at (100) and has al— ready been described. Both models were fit to give the ex- perimental n and then gave better values than the NFE model 111 for the eXperimental n . With g 1| to (110), the fourth zone 100 Open orbit layer has diminished in width, while the hole orbit layer has increased in width. This should result in an in- crease in the size of the two-dimensional region about over the NFE value in agreement with experiment. At <2ll> there are still orbits Open in two directions. Furthermore, on the AuAl2 model, there is a small band Of hole orbits on the electron sheet, which Offers a possible explanation for the suspected aperiodic open orbits near this axis. NO hole orbits were observed on the AuGa2 model. 140 We were unable to measure the two—dimensional regions of open orbits in AuIn2 due to the small relaxation times Of our samples. An approximate B2 dependence of the magneto- resistance was measured in {100} and {110}. The magnetore- sistance at (211) saturates, while at (110), m.~ 1.5. Hall effect measurements at (100) indicate that the Fermi surface of AuIn2 may be similar to that of AuGa2. We have presented eXperimental results on whiskers in AuGa2 primarily for later researchers who might want to compare two analytic models of the Fermi surface which give good fits to the experimental two-dimensional regions. In such a case, the extent Of the whiskers can aid in deciding (25) For the present they merely which model is superior. serve as an indicator of the large value of wcT achieved in G3. Summary In summary, the NFE model does not agree with the re- sults of the magnetoresistance experiments because it does not yield Open orbits near and because it does yield them in the region between (100) and . An NFE model with a radius swollen from 1.495(2Wh/a) to 1.552(2Wn/a) to give the experimental n111 in AuAl2 provides an excellent fit to the magnetoresistance data on AuAl2 for a sampling Of fourteen field directions. An NFE model with a radius swol— len from 1.495(2wh/a) to 1.532(2Wh/a) to give the experimental nlll in AuGa2 produces the experimental magnetoresistance Of 141 AuGa2 for most Of the fourteen directions of the field which were sampled. Therefore our magnetoresistance results give strong support to our interpretation of the Hall data, i.e., there are hole orbits on an electron sheet for g \\ and the Open surfaces Of AuGa2 may be more NFE—like than those Of AuA12. 6. Conclusions Extensive galvanomagnetic measurements on the AuX2 compounds have demonstrated the feasibility Of Obtaining rather detailed topological information on the Fermi sur- faces Of metallic compounds. In AuGa2 we were able, for the first time, to consistently Observe magnetoresistance ridges due to higher order open orbits, while in both AuAl2 and AuGa we were able to determine the angular extent of 2 aperiodic open orbits. Hall effect and magnetoresistance data in AuAl2 and AuGa cannot be explained by the NFE model. A modified 2 NFE model which increases the number Of fourth zone elec- trons better explains both galvanomagnetic and deA data. High-field galvanomagnetic properties primarily con sist Of weighted velocity averages over the open surfaces. Thus we have presented evidence that the open surfaces of AuGa may be more NFE-like than those of AuAle. This re- 2 sult is consistent with the OPW predictions Of section 1. The evidence available indicates that the Fermi surface of AuIn2 is similar to that of AuGa2. Relativistic effects may play an important role in this case. We have shown that our extension Of a single-relax- ation time theory applied to a NFE-like model Of AuX2 gives a fair approximation to the experimental magnetoresistance in the {100} plane. Perhaps, more importantly, we have demonstrated that for one complicated Fermi surface, the 142 143 magnetoresistance falls into the same three categories we described for a combination Of cylindrical and Spherical Fermi surfaces. LIST OF REFERENCES l. 2. 7. 8. 9. 10. ll. 12. 13. l4. 15. LIST OF REFERENCES E. Fawcett, Advan. Physics_l§, 39 (1964)- D. J. Sellmyer and P. A. Schroeder, Phys. Letters 16, 100 (1965). D. J. Sellmyer, Ph.D. thesis, Michigan State University (1965), unpublished. J. Piper, J. Phys. Chem. Solids_g7, 1907 (1966). D. J. Sellmyer, J. Ahn, and J.—P. Jan, Phys. Rev. 161, 618 (1967). J. T. LongO, P. A. Schroeder, and D. J. Sellmyer, Phys. Letters, 2§A, 747 (1967). w. G. Pfann, Zone Melting (John Wiley, Inc., 1958). E. Fawcett, W. A. Reed, and R. R. Soden, Phys. Rev. 159, 533 (1967). E. Fawcett and w. A. Reed, Phys. Rev. 123, A723 (1964)- A. S. Joseph and W. L. Gordon, Phys. Rev. 126, 489 (1962). J. P. G. Shepherd and W. L. Gordon, Phys. Rev. (to be published). A. C. Thorsen and T. G. Berlincourt, Nature, London, .122, 959 (1961). J.—P. Jan, W. B. Pearson, Y. Saito, M. Springford, and I. M. Templeton, Phil. Mag., 12, 1271 (1965). D. J. Sellmyer (to be published). J. Ahn and D. J. Sellmyer, Bull. Amer. Phys. Soc.,.13, 485 (1968). 144 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 145 c. Kittel, Quantum Theory_2£ Solids (John Wiley and Sons, Inc., New York, 1963) pp. 249-266. T. L. Loucks, Augmented Plane Wave Method (W. A. Benjamin, Inc., New York, 1967) p. 15. M. Kohler, Ann. Physik.§, 99 (1949)- E. Justi and H. Scheffers, Metallwirtschaft_11, 1359 (1938). I. M. Lifshitz, M. Ya Azbel', and M. I. Kaganov, Zh. skeperim. i Teor. Fiz..31, 63 (1956). [English transl: Soviet Phys. — JETP 4, 41 (1957)]. R. V. Coleman, A. J. Funes, J. S. Plaskett, and C. M. Tapp, Phys. Rev. 192, A521 (1964). w. A. Harrison, Phys. Rev. 118, 1190 (1960). I. M. Lifshitz and V. G. Peschanskii, Zh. Eksperim. i Teor. Fiz..3§, 188 (1960). [English transl:Soviet Phys. - JETP_11, 137 (1960)]. J. E. Kunzler and J. R. Klauder, Phil. Mag. 6, 1045 (1961). J. R. Klauder, W. A. Reed, G. F. Brennert, and J. E. Kunzler, Phys. Rev. 141, 592 (1966). M. E. Straumanis and K. S. Chopra, Zeitschrift fur Physikalische Chemie Neue Folge 42, p. 344 (1964). D. J. Sellmyer, private communication. D. J. Sellmyer, Rev. Sci. Instr. 28, 434 (1967). A. J. Funes and R. V. Coleman, Phys. Rev. 121, 2084 (1963). R. G. Chambers, The Fermi Surface (John Wiley, Inc., 1960) p.114. E. I. Blount, Phys. Rev._lg§, 1636 (1962). 146 32. L. M. Falicov and Paul R. Sievert, Phys. Rev., 128, A88 (1965). 33. I. M. Lifshitz and V. G. Peschanskii, Zh. Eksperim. i. Teor. Fiz..3§, 1251 (1958). [English transl.: Soviet Phys. - JETP Q, 875 (1959)]- 34. J. R. Klauder and J. E. Kunzler, The Fermi Surface (John Wiley, Inc., 1960) p. 125. APPENDIX A APPENDIX A The Harrison Construction Program This program is conveniently divided into the following sections: I. II. III. Read in Calculations A. Rotation Of lattice and zone boundaries B. Plotting Of zone boundaries C. Plotting Of Fermi circles Subroutines A. Matrix multiplication B. Coordinate elimination Definitions of important variables are: 1. 2. HOT is the Euler angle rotation matrix. THETA, PHI, and PSI are the Euler angles in radians as given by Goldstein. X are the coordinates Of the lattice points in momentum space. EX are the rotated latice points. VARRAD are the radii Of all the Fermi spheres at their intersection with the plane Z. AB and 0RD are the x, y values Of points on the Fermi circles. C and S are the values Of the cosine and sine. V gives the directions of the vectors perpendicu- lar to the Bragg reflection planes and the distance Of the plane from the origin. CE is the rotated version of V. 147 10. 11. 12. 13. 14. 148 KT and YT are trial values for coordinates describing the line formed by the intersection Of Z and the Bragg reflection plane. XX and YY are the acceptable values of XT and YT (those which are not outside plotter bounds) The two intersecting planes may be written ax + By + 7z = 5, z = 6; DE = 6-76. VOLBRZ is the volume of the Brillouin zone in units 2vn/a = 1. VALENCE is the number of valence electrons per primitive cell. SK and SY are scaling factors for the plotter. SX = .67 means that a line in the x direction of length 1.5 will be plotted with a length of 1". NC counts the number of cross-sections plotted in the x direction. RNC is the distance the plotter pen moves back to x = 0 after a row of cross- sections has been completed. NPLNS is the number of cuts parallel to B, i.e. the number of Z planes. In CALL PLOT(Y,X,n,SY,SX), Y and x are the values to which the pen moves; if n=1, the pen is down; if n = 2, the pen is up. Because the Harrison construction only requires a knowledge Of the crystal structure and the number of elec- trons in the conduction band, it is easy to adjust this pro— grammed version Of it to other metals by appropriately changing X, V, VOLBRZ, and VALENCE. This has been done for a body centered tetragonal metal (white tin) and for the hexagonal metals (cadmium, magnesium, and zinc). An adap— 149 tion of this program by Professor Sellmyer‘s students at MIT has calculated the NFE model of Aqu2.(15) L1 \ \ I.|IA. ill m-..§.-.u.-§ - - “a... 02!2A!AZ-1__. Liam PROGRAM CNEODQ 131' IE" ST0\'MR-3T(3 -3): VI 3-18-1-0'UTIIWEXFEATIUUTTVA'RRADI1'00)TLZIlay'm‘hm' [. DIMENSI0\ ABIIDQ). 090(100) V”’“"”“D[MEA510\ THETAIlOIIMTHATKI1UITMPHITIOIaVPHYIIO): ' ' DIMEI‘TSIO‘ C(180): 9(100) DIVERS-I 0\ ”WC; ( 3 .‘ 20.91:” “V ( 4 IZDVTF— DINEI‘MSICM GAQI2): ”5(2893) INTEGER- STFP..- QUIT-.WSE‘JTT'WGU‘A‘REo REIAD 1008,V0LHR21 VALE‘ICE T—_’1’U‘0_n FORI’IAT—n((5718:6’mflwn—“rufiw READ 630: 5X: SY: \IC 6 I) fijMO'P-HA TI'727r170-:3i,9-' I5 ) _____ READ 6-37nGA-QJ119 GAQ(2): NNN “-WW'N7TOC‘IMA T( 2 F13,‘; "15 )I It." -.--,-._....._-.._..._.._ L 1 FSIIIOTIWPSYI10) 'XTIZEITVTIEST,"XX'(ZS'ITMYYI'Z‘SI' ' "' m- -----— --. UB ~2CUTIWEADMZJIFC—THATAIIITmthIIITWPSVYIITWCWITI' ' 201a F0:MAT (3r10 .5. I1I _ __ —_ '- ‘I""' IF ('LJIT .FAI. 13"""10"TYI‘2011 I_ z I. + 1 __ ._ —“””"*“"" 00 TI 20“f”"‘"""'w __ 2011 NA = L - 1 _.--_- 11-1w_....__-._-__._-..._--... “”"fl-“IJIEI'TW -_.____-- "II—”"— -_. 2999 Penn 3900, (XII.JI. I= 1:31;__§§§I ..ii.”*w 1.11-11. —— ‘BCAR”F0?MA (s (Eridio; L21. 1) T8 ENT 'III ”GO. TO 3001 -~.—_..-_...._.....j '2: J17“ W“' __.-.....-_. I" - ______ _- 60 TI." .7909 __ - _ 1.1--- w m” _____,,_,, SanimeF":‘J‘J"I K = I “"me m--- __--.._.-. 11------ I.“ “"299 READ 399;'(J(I)KITWIM?“11M4II GUARD _, 30n FQHMITcariA.o. 11) __”* _-----.-_-l , “I" “I" ' “IF"(I-u'wj '21:".w1') I'EJMTO-3U~‘11 ____”___ K 3 ". + I _- _‘ __ ,_,,-....___--_._-__..-_-._-.i._.-..-.- ““ EC‘T' 291 ,__ - 301 \‘PTS : ,4 — 1 __ -1- __._ ml. M. _ - I ‘“"001v 3‘371A15926; / 150.0 “fifig READ Emi, HMII. 1==1'Z?X___- ..1 1-1.» - "WW-5‘91 FOvIvItT'I’BF'iIIAI """""" ‘M~m*‘“_ :IEAD 509, (SIIIIMI_?_1__Z§]___ ,u“__ 1 1-1 1 - 3 «a a: 7,4 5 LEIJIH‘T‘; legal—"(c.375/ _<.I_4_i_$f{_):__‘i_0'(_.ffe7rVAL__E’\ICEI .1-.. -1 ““ “““Jq”e"¢o., DHY(L). PSYU_m ”.JMLEWQL Q____Q__Q,Hw___uhmr.‘ 5410 FOTM£T(Ln 2, .2 :g' 76.3) ~~133m£.,-w“QR§erQNE_gq¢anARIES __W_M___ . _ ..LL-QLH- p INT 1,; 9 _-_ 108 F34MAT(31nx «I ( “waum_ DEII,_K) RIQ SflALme_§83~M“MU__ "“"37""””””””;*' 1x7~dy ”'vs xx XT(I) YT(I)*) ‘- .~_-“DD_2 CAI 5 I. IPTSH" w HJ_”Q E -w-w.r 1 ' : "4 \IN “‘“-—5-. .22-:P38;N_1AT;_PE=N3(KI 'QC_!.CONSIJ HHERE.0(KLNE.GARLK)Q!.DLH- UE(I.K) = GAJ(<) «1(4.I) - CE<3 I)*Z(M) ~-—-L;__N _ME ACE " I_v1w3 THE 9AIR 0F SIV_ULTANEO_QS EQUATIONS “,5 c ‘ Ax . a? . (z = a. z = CONST. THUS 1E CONSIDER THE VARIouS ' 4““-QA~M_QRQSSIBILITI55,A=Q:J. 5:0:. 9: 0; A. Mi. QQANDLR N-.-0.ELQWWM TF (CE(1.I) .=0. 0.0 .AND. CE<2.I) .EO. 0.0) so T0 2nd *--»_QQ__MLF (15(1 1) 50, 0.01 GS To 150- w.-_--_“.MEE mnflvnwnum_33wumu IF (CF(2.I) .Efl 0.0) “0 TO 140 '“‘-~—~_____QQW13N_J 5.1 L11LL”-_EHHE-mmAW- ,. ,r- —u~—u~ ”mm m» w—~ AJ = J “““ ,.E-m,-_._.HML-__ ‘5”. '-—-‘—...______ ..__ ——_...__.. .—._..A ---.. - ., -A.- E 7“ ,E .. ..... . -——* IwmsA *_,_ ---——.~.* -. a... 152 __.-0_2-[2 0. [6]...“- - _ -3.0 + AJ/2.o —— 13n vrsz IIIE‘I"I"."KYT":E(1":HTKTTUTI‘V‘T'ETz.II .-.-.-_ - C NE ELIWNATE UNACCE’TABLE VALUES 0F Y AVD DIMENSION A NEW -—— c vAHTABLE”?Y‘AHICH”5AEY“C0NTAINS“NN"KCE€PTKBIE“VALUES“ " ““““‘""‘ CALL ELI”NAT€(YT.XT.YY,XX,NN) IF "FF AFC—FEET”? 'I"'G‘e)*'°FT'3W1F‘DFO DO 131 J = 11231 AJ J YTIJI = -3.g :WAJ/?.0 131 MM) = muI.AT213571“???r233???ecI,I) CALL ELI”NATE(XT.YT.XX,YY,NN) _. C') N 0 ST FIFST-IWI ‘5: "C ‘4 AA I A] TA“?! ATE—_I F‘— T?" RFE’ I S—EFITIV "O‘N'EWKCQCEP'TFA’B'CE ’V'MA LU E' " ‘ IF I NM .LT. 2) GO TO 61 '5') NOV FE"FTND THE ”LA? EST VYFANU'TWE.§FACE:ST YY AND—DRAW AMIIAE BETWFEN THFI 10” O - VVYTT“T'” vv<1> BIG” SMALI “DH-O 5° K __ IF (CHEC/l .LT. 5.%) GO To 5389 538a PRINT §;L34.J_ __2_d_"_ ‘ -WWL“ 5381 FORMAT(1>. *CHECKl FO< J =*.13) ' 638° CHE-‘02 = we -.J._z._:_._.v.EEE_A.2.LJ.2 2-2.- IF (CHE 3r2 r. ~5.5) 30 TO 5110 530" PRINT *3“1_2l__ - _fl_ 5591 FOQMATtl), .CHECk2 FOR J =*.13) ' __ fiflmliwfifiifl -- —~»~~ 511n IF (VAHQ£D(JT .GF. 1.00) STEP = 1 IEMJNAfi9fQiJl.EBEJEJEDWJANDEMMARRADLJ) ELJAHJJEQAH_SIEB"E_ZW__w"-m- IF (VA3?IU(J) .LT. .50) STEP = 3 _ -.__.__- .230 52E? 1.;_51EE 22.51EP . ._____.M_HE ”m_.w_n- A8 = Fx<1 J) + VARRAD(J) * C(I) + 5.5 _.WHE_EEEELQPJLL1.;-EYKZLJIWEWMABBADAJIW3ESJI) +_§ES 2% CALL 9237 (3“0(72). 58(72). 2. SYISX) .___n_“*wm. n3 :21.__T ; qTEE, 22, QTEEH___, _ _“"“_,,Mwn 5209 CA; L p'jT (J‘U(I), AR‘I): 1; 5Y1 5X) “n ‘ --~n--o---.- —~WE_QZLLJXTW;M'EPM_ __2__m*wmw‘ u"_”“mmw__-*npi 5433 co=71une - _..__..._._____________ P_RI.‘."7_541_2 ___- ____ --_._._....._.. __ -- W2 , 5419 F3 niT, 1EF10.33 —-——__~-~~HNCEE K ;_HffiECKfljNJWEEW_-_.-g —~-—~~—-' "‘ IF (" CH:- .-F". .'3. NC) 60 TO 5499 -_ww__*_~§AL}HPL3TL11.E, -45.D.-21.SYLUSX) -«- ~-~~—~w~w~wu-~~~W'~W CALL PLJT (0.0. 0.0. 0. SY. SX) -- “III-h.- w--—.—wk!CjE: :K _: ml ~ - _._.......-.. "' ‘.- —‘ _ ”‘--__.____‘“~,- -_-.~‘—."Oil~-m-.'..‘" —---—*¢i '- GO T“ 53;, r} -—-—__.5£9°.Fu"2~'37 (i 9 L 0. 2, SY._SX1_ CA L 9')? (n ,0. o. n ,9V.SX) -iififl-£J,_J1f:=; 900“ C0 T!‘ ‘~»~~__«_""_QALL_ 3!; CALL PLi “_~*-* W W ~——————~——-.-—. ..._._,,7 - -.. o 5‘ ' -"-_-_._-.‘__ fin“ _l“(1 U ”’2 O. 2: SYISXJHh_", -r__mflmr“fln-w~wfl,-ww.w T (0.:.0.0.-1: SY,SX) \Jd “~— . " .— .. —— .—- _— ._..._ _ _..... ”E... .. ._ _....---. N I _ - _ --.. .. - .— _ - ————._ I ' 'J - ._._...._-._._ .. .. - A- - '~ -.-" " '--‘-- -—___.__- _ __._.--— n... .-. _- ‘-‘— _.___.__ -- - ——~...-—— *4...— 4...» w - __ _.._ __ . ___.._. -_ ”—..“.— K -- __-.. “—-.—_- - _.. ~—— fl.- .... .. .—. ' .—-- .— MMM- .- _. ..- o... w, _u - - '— h-o *— v- — ”—..-.4— —-— .. — an..- - .. -u’v- —- ~ m _ ___..—.._._._A_.—w.-_ .L-_..__. .4 M..- ... _. .— _. —._.- V —— .. _.. - - “ *,..~«. 7..- .-- b-"-__ ,,4, - "—"""' - — -... - .. . , “7-, ' ”A —~ -- *— ""‘— " - v .- N‘ a _nl- . u..- -f— “—.O- -0 —. g... ~— u.. “a. .n‘ .- .'_..- .. ————~ A... w. um ”_“~_gwmfi-_m_.Q212Q16ZM.w "r 154 fTN5.3 -_____m._"_u_._._1____-_-wu_.__ _r- __ SUGPGUTI‘E ”TQXML(?JT;XoEX.NLP.L) ‘ ”"' DI”EHSIO‘ INITISTSII'R(LBIHJYYF"EYTKTNC53 “‘”“"”'“' no 3010 9 7w“,,; # DO 3010 I. = 3 Ex (I. J) = q Q,wi . J. _ ._ III- I I I I .1. -- _ ~' H--- Ff, ' DO 3d10 ' = I 3010 EX‘I: J) : EX( RETUVEW.__"*- END 3 .9) + ROT ‘ ' H“ ——~——.. . . ”4* -——.——~‘—.—_—-._- .—__—. —— __. ——.——-m .— ——._.~ _. ,_, fl.— — - - _- _ .. _wa _— JV —.‘N~_~_ ”m —- W...” .. ._ - q ’_ _ ____....,_. .— A. ‘W—mhfi—«M fi ".- .. m~m ”M... w ~._ _..- .— —— -w” . .. .—._.- .— -ow.--~-. ~C~~M- «tau—— . , w- A $.o-— vi} ‘Wq—n— .-...--........,._. .-... .. .--_- _VH _. --....— ”w- 4."- -.4 . m-“-‘d’ alt-I" - ~—' ‘V‘ 1.11 I . I . . I I 'I.|| III III ,1.Ifs I. :| -mqmoac mnmn.cL-;.mmmh.c r:::-; II-r:: I;;,-II.IIII-IIIIIIIIIaomnfiu¢:I-IIVoocuc-.-: cccocc.v u wzcx .a; ho wzago) ‘3'. [Oni'Itl I.‘ I I . "l‘i‘. Il‘lu. I cl ‘I ’l}- .I I Ill. 0 .1. It! I'll-"Ill III. I ”E l . I. 1 y.|..[ [.I‘ll II!!- . ‘lnlit‘l’l'lllllll ll.‘ II If -1 I'Ivl, ,u|:.|llll. ,.A|I.l III , II I 23SamHm.z.ou-..zcm5:1,m: . , - III}.,I...--I-III 41‘ {lilt’ig I." G‘- ‘l'll 3....» , Ii... .Ao.o n va p smacks» use a 09 case: omupoam noapoomammOQo was .30Hmp cocsaonfi ma Aooav scam 00H 155 madam heady 0:» CH m.nom awawonn man» 59 came maoapwasoawo no psalucfinm d nmuv) § ~I‘ h la zit-.1 ‘ --.I --III:;II- tiégzconv-fln i mflfioym:IIIavevsHhIszlszal::zscecc.fi- NamN .- O zIIIthsocmroH-I-IIIIIIV-mm~.$ .-Nl C D Q :- o H it‘lllll‘tIC-Qi-i" t I‘ll-lulu; $43? lit-311;» smOVJOIIIIfiamo.wniizmvfivnfl l I'll-‘QIIII‘EI. In!“ I) I‘IIII'IIIIVI iI2IIIIII-I-i:;i:1i:-:I:comYmaIiismaaoaNuIiINvflwwfl -Izsrcooz.a comm.a fioam.fiu vmmm.m :cce.a IIIIIISIIEIIIIIIIIIEzIIoocoJawliimfivmonIIIvmmmHm. cc:o.NJ- coco.a vam.o vnmm.wt cocc.m I .IieIéimcoc.mnIIImmmvumIIIIccccmcc -Ic;Qoqxu: mmnc.fi mmmfi.n cco=.o. age: I I mwmv.awaiimmmflanflilfcccowo cocs.mu - mocv.~ mmM¢.m- coco.o ccoc.m IIIIIIIIIIIIII-IEIIIIIIoooowHNI. nxvaoMIIIvcmmwm .ocuo.mJIs coco.a I-mx¢n.o vmmm.m ccoc.m vmvpnflslxumvac.w. -cooo.m- mmfim.mw on" ovum.a ocvn.a mvfiv.fi- zooo.m, ccmmMfiwllicovNWflwlllthvHM coac.mu mmfim.m vmvo.a- «Vfi¢.fi cocoam-, mvflvww. ,. ccoo.mq- I..-“ ”m. II;III;c¢mm.Hu:IIco¢anu l mmrm.m vmvo.a. mvfi¢.fi. coco.m ,mmfim.mnttsvnvcnflIIIINVfiNwfi aecawmn ovmn.a oo¢n.fl N¢H¢.~ . coco.m -: ooooflb:tsacooouo- ¢mmmww4 o:co.o «Hov.o. mnmn.m occe.o- Icqeo.cI mfiov.o mnmn.m- ecoouo cccc.o .I'l'llllll‘ momm.o ooom.H occo.o. cooc.fi -N00m.o1 vocmwdfltIIcccowo IQCcD.HJ '1! ‘.r. ‘II II- Illll‘lll'. , II I. III!" I’ll! ‘lull comm.“ Hofim.fi. coco.o ceoa.H mvwoJQHIIIonNfiwouzisu¢fivwa caoowfi. memo.o onNH.o mv~v.« coco.a .co::.mu- eoeo.a, mkvm.o occc.o coco.m -xmonunnziiwvavwaucsIIs:s-:::;-coco-a cm¢~.o.. “mom.fl N¢H¢.H coco.oy .foooo.ar nkvn.o. .1- II 1 II II.) u IILGII'IIVI II'VS!I cooowb U‘III'Q‘D’ - I ‘I It‘ll} .- I III. I‘lII omcmwo, omvmnbwilihwonha NVanflu I I.‘I'ulln -Iaagzwg.-.n.mnguazIr~wmw:I .nym I . I . . MFKIMFZPDQIWDFFFkawI» . . _-. Icccs.ané “mov.o aomo.m nv¢¢.fi- coca.a Iboco.fiu. nomn.ot voom.fi- comm.“ cooe.fio :as:c.NJs rcccs.m: .iIII:c;o.mo Inm \‘ 8. III." I coco.o.. coco.o vmmm.m ococ.o mvma.oniIIonnfiwoullimvavaw . coco.fi- coco. mvmo.a ommfi.o mvfiv.fi. coco.H:II- . , ;¢omm.auIIIHoH~wa.surooopwou. Icoo=.a. macs. Iszicczo.r H>ur-M.4r1avqa;mrvaum:va:m -cooo.m4;--:cco.c . . - ,::;:::::;ésg:acse.o. omvm o umom.a. uvflv.fi ooco.o I -IIcPPPPPIIIIbpbebIIIIbbbbnb;irp{Iiiigi accomao;zgrbooo.c 2:-écoacufif‘3;:co:o«mw in; - I I --.s- -.-.iI-I--.m.m.v x ,1,.,I.I .r’) CC;O.«:..I NV £3:¢;o.nwi!:vc;IiiI :cc:.mu cv Ia;c:«:u.n;iII-3nIlIIlla cccc.m rm coco.» ;fIxn-1:II1 -- acne.» rm - Izcssowxulifmn cc;c.ma vm I -I IIIco;:.mMIIImeIIIII-II cccc.mu mm ..-::co.ms;tifin:s: :caa.m cm -IIII,1 -:::a;o.m-;- ow coco.m IquIIIII::II I. ‘IICOII. 52:01“- LVN ....... slut-I. P:c:ra.ae- am c:E:.m -1uvm.IIiIIIII c c r... o . c IIlss mm ccao.c mm::IiIIII- I! c 3 _.,. 3 . c it N. :ccc.o .om I -.C::G~NI 3d ccco.mu ma -;zco.m1 AH cczc.m I510flieIII ;I ::-::;a.flJII:$HI ::co.ws VH 23:3.a1- ma :ccg.~u;;:wfiw- :qc:c.a M” c o z o . «II: -;-c w;- I‘III'IIJII.’ -l.|‘t:li.o-"l|l. I. cos-o..~ cap-Aim- :egm.c coco.o ~".~’ m A c -:§I;m- v m A caco.m I? .c at Pro--- {HE [‘51 {iii}, .wvx .I. If ‘I lit I .I.." I I’I-Iil’l v.‘ I [It 1"; AI’I: I. I: (I l! L) I! I} l) nnun (I " (I " .‘1 ll 1) H I II n n 1. .5 I a . a a - I II-.. 4... 4...- - -..-4:... . ...-II-4.%N4...m-I “mm-...... “....M. .m----......... .... S... . ..-----.-- ...-.... ...-.- ---.-,..,.......4 . . . onw.c 0.. -lIlII -- I ...-IIIIIc.w.4 ovx.c n. . I -.-.-M-ww-q-T-I-Iwmw.m IIIII Icon. 4- - 32m” 4. ovmuw .43.... 4. 4.4.3....- II- 4.4:. ....a... - I “Mm-...“...I Iwmw-..44-III CDC. 0 o oo. cI-III- c o c 4 c-I--I.I.-- coo-.144..- I-Ic ot-fiw-IIQ-Qc .-c IIIIII tenfw-II-II cc: 4 - .4. 4.4. 4. . 4.4 440.44.. c. I-ooa. o mov.4 A44 4 m4¢.4 mov.c mx4 4 mm4 ova. cq-.x-III:4:,44I-I- «VII-cm. 44 £44 . -4--I-I- I m 4....4 III-I-o-ob-Iic- - - Iicoc m.~.....I4-I-I-Im-m-4.-.. 4---- I Im: .4 - - 4m: nmm . 4 IIII I. umq 4WHO.<.mm III-II III-IIII-I-III4.44.-...mIIIII4-IISE . 4 ... 4.5.4 .-4..--..---.%o.a IIIIII 4.4.... 4::- - :54 ....... III 4. cm. 4.. 4 pom-.-..m 3. Oman-m...- -4.-4-. 4-..-.4, 4.4.... 4 4 4... IIIIIII-II-IIIII-I-com. --4 0 com...“- 4 99...? 34. 4 I 4.9... 44-II-I-II I4I:-II~...II--I- . com. m IIIo.-IIIII com .-..4-wI I4 No .4-.H-4-..-.-I-IIomo ..m .43.. 4 4.- III-.4-4I4..>IIII I--.4.4-.-4.x-I-I I4mz4x-xI m2 III-.3244; m2 ...:Em 3m - -5 -4... .414.- -I. ,4. I -..I- III- -- .- II-IIIIIIIIII-IIII- II- 4.4:.-. .-..o-IIIIIN -54 IIIlwmm4. o-uI-I¢_ooo-..o-III4N-o-4IQI coco-4:1 -cocc.-4.II-II-..4:.4.. .---.- -..4...4...4 I4. III-III l mNNH. o 4wen-40.04. 4.x.c-m.o coo,o-.4IIIII4E:D.4-. 440444.45 c4440.4 4. II -mmm4. oIIIIvooo.okIII44cNI.I 403014 coco.c- coco. II.cc.c.e IIImIIIIIIIIII 84.4...-4-4I4-mfi-4 42.4... 4444.4 ...-4.4.-..- I--.:....-.-.-4-I-_, ...-......4... . “-..-osiII - - ., I III-IIIIIIvvaINII ocmm OHIIInV4v.4I scansnI-I-CO4C.4 4 I Icc.o.4-IIIwnI-IIIIII amen-NII 54-4-0. HUI ccco. o COG-a mute-III pace. 4.... 44.4_.4.o.m xfl. 449cm.va m4; Io IcochI on 2:44.. w... 444......4 -II. ....4..a.4--IIII mow-II vvmo.NI. comm.ol wVHV. H-I-I-I-III-I III- cscs. 4.3.24.4 44.4.40. 4 on IIIII - IitIlIvvma.NIIIIoomn.aIIIIN¢4mw4I I- -ccoc.n.II cccc.4I:I ::.c.4u:I--hnIIIIII-I 453.4, I444... 4......I 4.4.4.... 4. -.--.-3-IIII- 44.43...” 44......4- 435.4 I. -IIIIIImmc4.m I4n4o. 4 cccc.. c- cccc.w. . coca-4:-I cc.o -I-I,nnI ...... -III «cmo .m .0omm. -o «V44. 4 coco.4.:::.e:4.4IIII (4.3. 4.. IIInnI mom-4. 4.....II 2.44.. -4. 342...? 2.2.4.. 4.4.1....- 4.... 4.. 4.. 4... I snow. ouI-I 4omo. -mHIIIuv4v. 4II- IcccaJ4.IIIcoccwwwII-CC.O.I4 an «4.2.4: 404“. 4.. vex-c .m. 4.95.4 ...-4.2.4..-- .4... ...... 4.....I-I-a.¢-IIII out. 4 4444-0... ~HI.-.n.¢4v-.I4I 4:54. ..4 -II 2.4.4... ”II-3.4...44...--4: I... «-.--III- -.II-II-IIIIIIccuv; 4I... $440-. N N44444:.“ ooco.4| coch-W 3.4.5.4.: :4 comm-w4-nI4 o4-m..-4III.-I-vmm-m ...m 4..4.........-4-.I-.3-- ... 4. .. 4... .-----.. .4... .... ..4. .III-c.4...I-I nnov.o 4omo.m mv4v.4 coco.4 cczo. W ceco.4u nv I -- - mon4.o.II¢-oom-.4--I-I-I-vmmm.m-.-II- II- . 4.34.9.4 -.. 4.4.... ..4- E. 3.4 I. comm-4.. IRAN-.4 vommImI I IIII-I-o.o-S..4I - 4.9.4.. 4I--.-4.o-.-.o-..n.. n... .| I I.-ll IIIIIIIII'IIIIII APPENDIX B APPENDIX B A Program to Calculate Ap/p in {100} for AuX2 The terminology in the program is obvious, e.go: u MU, pxx = ROXX, = VZA, dpz(A) = DPZA, (uvxu> A B MUXXB, etc. Note that the factor 2 in equations H1 is hidden in the statements following statement 32. 158 .. - - _—.--. .— -..-..—.. ---.- »-- . _ -- _,.___ 7 --- -..—J- -... - o- .. _ fIN503ANlliiu-u. V159 "-»a-:.£:~-a. ‘---‘.--—¢ . - .‘ v.-V.. ~ 7‘”- PROGRAV FOURBZ _ ._...—. --.-....-- “”“""“"””‘1”MUXXE. MUVXH, MUCH. MuxxH C ' m"" ""°”""PRINT 15 ' 15 FORMATtlHi) m "”‘"m””'*”00”40'v 2 1,45' ‘ I N "_““"m*"“” "PH! E 5&3.14159/180,n s ufsxvcth) ”“““‘C”-JCos Y I 8/6 “_——~— .N c .—..—»..-> ..«uuw. - _ - .. . _ H. 7“ » . - ,i C OPEN OQBITS "fiwmwuw‘_hM~V2“= .50(3,0*C/5 OSIC’ DP 3 02.0 'V‘mawwvflUVXA's’v1.0/( 8.0*C**2) ~ VXVZA : S/(8.0*C**?) -mufmvjm"*”VXVYA I 91,0/(8.0*C) WUOA 3 1.0/S * 2.0/(3.0*C) DPZA = S/2.0 V29 : .5t(¢-3.0tS)/C + C/S) -- - . V—_‘-* “09/29/68 “-m“vhn.i.l. MUVXB s .(1.0/(12.n,c)).(1,o/(2,0*C) + 1.0/S) VXVZB 3 '1.0/(8a0*5) ”WVXVYB 8 VXVYA nuns =12.0/3.0)r(2.0/C + .5/5) DPZB : DFZA A VZC : (92,0tS)/C ”UVXC : e.gtMUVXA VXVZC 3 4,Q*VXVZA “'vxvvc : 4,0«vxva “uac : 8.0/(3.ovan 'DPZC12 = DF’ZA ‘ DPZCS 3 ,5¢(C-S) “NV201 = VZB Nuvxfii = -c5.0/<12.0*C)>*<5.0/<2.0'9’ ‘ 1.0/S) ’ VXVZDl 2 S,O*VXVZB VXVYDl = 5.0thVYA - ' WMUODi : (2.0/3.0)tt4.0/C + .5/5> DPZDi z DPZA "‘“VZDZ = VZB ‘_W1.c,) vxvzoz : (..25/S)t(C/(2.G*S) + 1.0) ““VXVYDZ =1..25w(.5/S . 1.0/C) “U302 ¢ 1.0/3.0)a(5,o/C # 2.0/S) ““ DPZD2 C/2.o - S «urxA -1.0/<72.0~C*o3) ’““““"“‘“ wuxxs wuxxc -7.g/(18.0.Co*3) OZL‘: 1.0/(4.0.5) « 1.0/(2.0*C) ‘””‘ “' ‘“‘ “flU!XUZ = _n2L*,2*(2.o/3,0)0(32L/3c0 + 1 XMUXA a -MuxiA * “xnuxs : -Muxxa O. '1.0/(°6.0*C**2)*(1.0/(3.0‘9) * 1.0/S) '“**“wuxx01 - =n5.0/(96.0*C«*23*(5.0/(3.o*C) * 1.0/5’ .0/(4.0*S)) "YYPE REAL HUVXA. MUOA, MUVXBL MuOB. MUVXC; Huoc, MUVXDI, MUDDl. 1 Muvxoz. Muooz, MuxxA. muxxB. MuxxC,flMuxx01. Huxxnz. HUVXE' HUGE, nuvxpz =—<1.0/2.0)c(1.0/s . 2.0/<3,0~C))w(1.0/¢4.ots) + 1.0/(2.0 ”__-.._7______~_,-__.,___,-.._we -.,._.._ l- .. -.,-_,-..,. .. - w 160. a. _ _. -.... -- l. - [quJA‘MWEMW-~_M__."WlWMmHHHHso“,..H-. .. m a Mn . . -l 09/29/¢8 ”...—......— ””-"“*iflux01 g .nuxxni“‘ c“, ”"”CL03ED"onssz XMch : ymuxxc - XMUXDZ 8 BHUXXDZ VZE : 0.0 ”HUVXE x 91:0/(3.0tCti2, vxvze a S/(9.0~C**2) -. cw. ..-~-—-- ~ ... _q...‘-l_......._, ‘-.~~ -,. v- ' um-.. .—V_-. ‘00 I ”—... .....- " DPZE“5'0.5.*DP102 XX : {-HUVXArt2/MUOA c HUXXA + XMUXA )tDPZA - 15”<”9Muvxs..2/~uoa - HUXXB ¢ XHUXB)tDPZB ‘ '“ “ 1. C-MUVXC«v2/MUOC - Huxxc + XHUXC)¢UPZC12 16“¢‘enva02..2/MU002 a Huxxnz o XMUXDZ )tDPzDZ CLOSED oasrrs“ . -.Wmivyc g 0.0 le-_la ”i A‘.H.H _n--ufl , il.lim 220 x (VZE..2/MUOE)cDPzE ¢ .39 ¢ .2: VIC i'0§0 ' " ' XYC : VXVYErDPZE ¢ .39 c .25 -'XZC’= -(VZE9MUVXEtHPZE)/MUOE * VXVZEtDPZE XXC 8 (GMUVXEtt2/MUOE - MUXXE + XMUxE)~DPZE + .39 ¢ .25_ 'GO TO 29 _ “ “ ‘ ‘ ‘“ ’ ‘ ‘ no i 22 YY : _ ”‘22 = VZA‘tZtDPZA/MUOA ¢ vzathtDPZB/MUOB + VZCtthDPZC3/"UOC i Y1 = DDt(v7A¢DPZA/HUOA o v28*DPzB/Muoa ¢ VZC~DPZCSIMUJC) ' “W*”xv aecopoMUVXA/MUOA - VXVYA)*DPZA -'(DPtMUVXB/MUOB -VXVYB)*DPZ8 ~ 1(Da-PUVXC/Huoc =.VXVYC)*DPZC3 ""xz =-(VZAcHUVxA/MUOA-VXVZA)tDPZA - tVZBtHuva/MUOB-vXVZB)tDPZS - ' —.. '“OPEN ORBITS D°**20( DPZA/HUOA + DPZB/NUOB 0 DPZCSIMUOC) I“ 1(VZCoHJVXC/HUOC:VXVZC)rDPZC3 ' "xx = <-MUVxA..2/MUOA «MUNA * XMUXA "DPZ‘ 1* ¢ ~Mdvx9..2/uuos - nuxxa ¢ XMuxB)&DPZB 1‘ (~PUVXCto2/MUOC . Muxxc + XMUXC)'UPZC3 3L?SED ORBITS ‘YYC : “'0 . , -. . 21: = (VZEot2/NUOE3tDPZE ¢ .39 ¢ .2: YZC : 9.0 ‘ X7: 8 VXVYEoDPZE + .39 u .25 " XZS’: 6(VZEtWUVXEtDPZE)/MUOE * VXVZEwDPZE xx: : c-MUVXE..2/Muoe - MUxXE f XMUXE)0DPZE . .39 . .25 ' "GO TO 29 C C W ”'29 '60 51 PRINT 30. H. YV. ZZ._YZ: XV: X2: XX Foamnrc/x. 110; 6F10-4) "PRINT 3;. vvc, zzc; vzc. xvc} xzc. xxc 704MA1¢/11x. 6F10.4> ‘YY = YY + YYC 22 = 22 . 22: "Y2 = YZ o YzC XY = xv t XYC "X2 = X2 0 YZC XX = xx . XXC 32 '3RINT 32. vv. 22. V2? XYi X2: XX FO?MAT(/11Y. 6710.4) 'YYZZ = 4.0.YYaZZ ZYYZ = UYZtYZi4,0 ' vvzzxx - vvzz.XX*2.0 ZYYZ'XX’ZGO -‘fz..x‘(.XZ~8,0 YZXYZX _ 9YY3X7.*XZ'800 Zszxx YZYYZX Zszvx ‘YYZXXZ 162 _ ___ ... - , A 7 -,‘ A . l - 7 -- . ._ _ ,... ... , - ‘._ .7- .. P......- .. ... , -» -u-—~.—_—-..__.-. ‘ -.-~ - . . ETN5.3A---.MmH www~_- _06/29/68 "~zlxin;?i-22txvrxytsio c PRINT 38. vvzz; zvvzi vvzzxx; zvvzxx. Yvazx} zvxzvx. vyzxng miwmw-,mmm122xvyx -.7-. V -. L . as :oaMAT