GALVNQWGMETE'C ENVESSfi-GATW @133 THE FEM! SURFACE GF AuSn. lesés far the Degree cf 9’51. D. MICHiGAN STA‘E‘E UNWERSETY [>73va 1. Seiimyar 39:65 THESIS 0-169 I r71 ‘0 fi "f if '..’ A. In; Michigan Stat. University This is to certify that the thesis entitled GALVANOMAGNETIC INVESTIGATION OF THE FERMI SURFACE OF AuSn. presented by David J. Sellmyer has been accepted towards fulfillment of the requirements for Ph 0D 0 degree in Phi? 8108 M WV thor professor Date M ABSTRACT GALVANOMAGNETIC INVESTIGATION OF THE FERMI SURFACE OF AuSn by David J. Sellmyer The topology of the Fermi surface of the intermetallic compound AuSn is investigated using high-field galvanomagnetic measurements. The re- sults indicate that AuSn is a compensated metal, that there are Open orbits along the hexagonal axis, and that there are open orbits along <10IO> directions. A tOpological model of an open sheet of Fermi surface, which is in agreement with the above observations, is prOposed. Certain dimen- sions of this model are deduced from the Hall co- efficient. The quantum chemistry and electronic structure of AuSn is discussed in terms of valence bond theory and simple band theory, i.e., a single-OPW model. GALVANOMAGNETIC INVESTIGATION OF THE FERMI SURFACE OF AuSn. By ‘ \ \ , David J. Sellmyer A THESIS Submitted to Michigan State University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Physics 1965 Acknowledgements I sincerely wish to thank Professor P. A. Schroeder for his interest and assistance in this research. In particular, his help in the preparation of samples was indispensable. I am indebted to Professors F. J. Blatt and M. Garber, as well as Professor Schroeder, for pro— viding the necessary support for the completion of this research and for many informative discussions about various aspects of this work. Financial support by the National Science Foundation is gratefully acknowledged. Table of Contents Page 1. Introduction 1 2. Theory of High-Field Galvanomagnetic Effects in Metals 9 Dynamics of Conduction Electrons in Magnetic Fields 9 Kinetic Formulation of TranSport Problems 12 High-Field Magnetoresistance and Hall Effect: Closed Orbits 15 Influence of Open Orbits 19 Summary of High-Field Galvanomagnetic Properties 23 Rules for Compensation in Intermetallic Compounds 25 3. Preparation of Samples 28 Metallurgical and Sample Analysis Techniques 28 The Achievement of a High Degree of Order in Intermetallic Compounds 36 4. Apparatus and Experimental Technique #3 5. Results and Discussion 51 The Crystal Structure of AuSn 51 Magnetoresistance and Hall Effect 51 Topology of the Open Sheet of Fermi Surface of AuSn 69 On the Electronic Structure of AuSn 74 6. Conclusions 78 iii Table of Contents (continued) Page Appendix A 80 Appendix B 82 Appendix C 87 Appendix D 89 References 92 iv O\U1~F-‘\Nl\)l—' 0 IO. ll. 12. 13. 14. 15. 16. Figures Cyclotron orbits in a magnetic field various types of closed and open orbits Part of a cyclotron orbit Rotation of coordinate system Partial phase diagram of AuSn system Phase diagram of non-ideal intermetallic compound AlBl Graph of resistance ratio vs. impurity content for metals Schematic diagram of apparatus and circuitry Diagram showing sample size, shape, and potential probe placement Sample holder and rotating apparatus Crystal structure of AuSn Direct and reciprocal lattices for hexagonal crystals Partial standard (0001) stereographic projection for hexagonal crystals Graph of Ap/p vs. magnetic field direction for AuSn I. Graph showing approach of magnetoresistance to saturating and quadratic behavior Log-log plot of Ap/p vs. BR for AuSn I Page 10 11 16 24 37 38 41 44 44 45 52 53 53 54 17. 18. 19. 20. 21. 22. A1. D1. Figures (continued) Graph of AP/p vs. magnetic field direction for AuSn IX. Log-log plot of AD/O vs. BR for AuSn IX Hall voltage vs. magnetic field direction for AuSn IX Stereogram showing current and field directions for AuSn III and AuSn VIII Graph of AP/D vs. magnetic field direction for AuSn III and AuSn VIII Topological model for the open sheet of Fermi surface for AuSn (not to scale) Schematic diagram of Bridgman Furnace and electronic control circuits. Simple compensated Fermi surface vi Page 59 6O 64 66 67 71 81 91 I:- My " I. II. III. BI. BII. BIII. Tables Page List of semiconductors and metals 6 Summary of high-field galvanomagnetic properties of metals 21 List of AuSn crystals grown 33 List of AuSn samples 34 Crystallographic angles between planes (hlklll) and (h2k212) for arbitrary c/a 82 Crystallographic angles between (001) and various planes for 1.10 S c/a S 1.90 8} Crystallographic angles between (001) and various planes for 1.10 S c/a S 1.90 85 vii 1. Introduction The last decade has seen great advances in our under- standing of the electronic structure of elemental metals. The stimulus for the large amount of experimental and theoretical work in Fermi surfaces was, to a large extent, several developments which occurred at about the same time in the late 1950's. These were: (1) the prediction by Pippard(l) from the anomalous skin effect in cOpper, that its Fermi surface touched certain Brillouin zone (BZ) faces, (2) the explanation by Lifshitz(2) and coworkers of the curious high-field galvanomagnetic effects in the noble metals, (3) the observation by Schoenberg(3) of the de Haas- van Alphen (deA) effect in copper, and (4) the realization by Gold(4) that he could explain his deA periods in lead on the basis of a free electron model sliced by zone boun- daries. The exploitation of the nearly free electron (single-OPW) model by Harrison(5), in particular, has im- measurably aided the interpretation of tapographical ex- periments on polyvalent metals. The success of the high-field tOpographical eXperiments such as the deA effect, high-field galvanomagnetic effects, magnetoacoustic attenuation, and cyclotron resonance, de- pends upon having long electron mean free paths. For this reason the experiments are done at liquid helium temperatures on very pure metals. Typically, the impurities must not be -2- greater than about 100 parts per million. This means that the topographical experiments can be performed on random substitutional alloys only if they are very dilute; in favorable cases, however, dHyA oscillations can be seen in alloys having as much as one atomic per cent solute.(6) There is, however, another class of metals, 23g2_ metallic intermetallic compounds, which in.principle satisfies the criteria for observing the highefield effects. By definition, a binary intermetallic compound is a.mixture of two metals which has a well defined stoichiometry and atomic arrangement. That is, it can be written as AiBy where x and y are integers and where the A and the B types of atom each has a unique set of basis vectors in the unit cell. If one could,in practice, prepare an intermetallic with perfect order and with x and y exactly integers, then the potential would be perfectly periodic as in the case of a perfectly pure elemental metal, and the electrical re- sistance would approach zero (apart from electroneelectron collisions) as the temperature approaches absolute zero. The work of Pearson and coworkers(7) at the National Research Council in Ottawa, Canada, has shown that inter- metallics can, in fact, be prepared with a rather remark- able degree of crystalline perfection. That is, they can . 9(295°K)/p(4.2°K), which approach those for pure elemental metals. The recent Ill be prepared with resistance ratios R -3- realization of this fact led the NRC group to investigate several intermetallic compounds with the deA effect.(8) Although there has been a considerable amount of re- search on certain semiconducting III4V and II-VI compounds, there is relatively little known about the electronic structure of metallic intermetallic compounds. The work that has been done has been primarily crystal structure determination(9), and the correlation of certain recurring structures in intermetallics with electron concentration, i.e., the HumeeRothery rules for electron compounds.(lo) For example, the intermediate phases Aan, Cu3A1, and CuBSn all have the body-centered-cubic structure and, assuming the usual valencies for the individual atoms, all have electron per atom ratios of 3/2. That the area of inter- metallic compounds has remained relatively uninvestigated is due mainly to the complexity of the chemical binding in most intermetallics. In general, the chemical binding is a mixture of ionic, covalent, and metallic binding. To give Just one example of this, the compound NaTl is a reasonably good conductor, has an cpen, valence-type structure, and exhibits ionic charge-transfer in its NMR preperties.(ll) Chemists were successful in developing valence theory and in discovering the quadrivalence of carbon because there exist many simple compounds such as Cflh and CH301 in which the carbon atom apparently is attached to four other univalent -4- atoms. However, intermetallic compounds have resisted such attempts to construct valence theories because a given.metal will often have a different apparent valence when it is in combination with different metals. In fact, even in a given binary system, the two metals will have different apparent valences in the several compounds they form. For example, in the mercury-potassium system the following compounds exist: KHng, KHgS’ KHg3, Kng, and KHg.(12) In spite of such difficulties, Pauling has at- tempted to correlate a large amount of eXperimental data on interatomic spacings, magnetic moments, etc., with his valence-bond theories of metals and intermetallic com- pounds.(13) Physicists, on the other hand, have had the most success in understanding electronic and other prOperties of those metals which in the atomic state have a known number of s and p electrons outside filled shells. In- versely, they have had the least success in understanding the prOperties of the transition metals where it is not known, a’ riori, how many of the atomic d electrons remain localized and how many go into conduction bands. Inter? metallic compounds are similar to transition metals in the sense that it is difficult, in most cases, to predict how many of the valence electrons go into conduction bands. In fact, it is not even possible in many cases to predict -5... whether a given binary intermetallic will be a metal or semiconductor. In this connection, it is interesting to consider the list of semiconductors and metals in Table I. It is seen that for the group IV elements, the energy gaps decrease until metallic behavior is reached, as we go down in the periodic table. This behavior can best be explained on the basis of the ”Phillips' cancellation theory”.(lu) If |¢k> is the state vector of an electron in a crystal, then 2 ‘%“ + V Mk) = Ekl‘hc) ’ where V is the periodic potential of the lattice and the other symbols have their usual meanings. In the Spirit of OPW theory, let l¢k> be constructed from a 'smooth' part Ik> minus some orthogonalization terms: ”’18 = Ik) - Z lnk> , n where = m;(r) represents the core levels. It follows that the equation for lk) is 2 --Jg--m--+’\r+vR Ik>=EKIk>, where VR is a non-local repulsive potential, VR = ; (ELK-En) Ink> : V(r) [6(r - r') - Z] . . cor levels But note that 2: = 6(r - rt) , all - , states so to the extent that the core levels form a complete set of functions, the true potential will be canceled by the repulsive potential VR in the region of the cores. This is the basis for the remarkable degree of success enjoyed by the nearly free electron model in polyvalent metals. In the lower Z elements, therefore, there are fewer core orbitals in which to eXpand the delta function, so that the remaining effective potential (V'+-Vh) is a decreasing function of the row number of the periodic table -- from C to Si to Ge to Sn to Pb, for example. Thus the lower Z elements in a given column will have stronger zone boundaries, larger energy gaps, and greater energetic advantages for forming valence—type structures rather than metallic structures. These ideas are borneout quite well by the elements in column IV of the periodic table - as Table I shows. The purpose of this digression is, however, to point out that we see from the table that the very same thing happens in the IIISV and IISIY'intermetallic compounds, as we go down -8- in the periodic table. Such trends suggest that the OPW approach might work in certain of these compounds as well as in the elemental metals and semiconductors. To the author's knowledge, however, there have been no OPW cal- culations of band structure in metallic compounds. There is evidence that the single OPW method does give a first approximation to the Fermi surfaces of B' - CuZn(16) and the fluorite structure compounds AuX2 where X = A1, In, Ga.(17) In summary then, we have seen that the whole area of metallic intermetallic compounds is a little-investigated one and that the possibility of determining the Fermi surfaces of these metals has been demonstrated by the ob- servation of the deA effect in several of them. These facts have stimulated the present galvanomagnetic inves- tigation of the Fermi surface of AuSn. 2. Theory of High-Field Galvanomagnetic Effects in Metals Consider an experiment in which a pure metal single crystal is placed in a high magnetic field and the re- sistance of the crystal is measured as the magnetic field is rotated. It has been known(18) since the 1930's that a plot of the resistance vs. magnetic field direction contained a remarkable amount of detail. This behavior remained a mystery for decades until it was explained theoretically by Lifshitz and coworkers(19) in 1956. In this section we outline the theory of high-field galvano- magnetic effects in metals to demonstrate the kinds of in- formation obtainable from these effects. we follow the Chambers<20) formulation of conduction problems as applied by Ziman(21) to galvanomagnetic effects. The theory and practice of these effects have been reviewed by Chambers<22), Pippard<23), Baratoff(24), and Fawcett(25). Of these reviews, the article by Fawcett is the most complete and up-to-date. Dynamics of Conduction Electrons in Magnetic Fields The equation of motion of electrons in a magnetic field §,along the z-axis is e n E. = Tc (.Y;~ X E) (l ) where _ -l . ‘XK, — h vge(§) (2) -9... -10.. This means that the electrons move on surfaces of constant energy in k,Space and that the change in the wavevector is normal to §,and normal to Xk which is itself normal to the surface of constant energy. Thus k,is confined to an orbit which is the intersection of a plane normal to §_and a surface of constant energy. If fi'is the component of k,in the x-y~ plane and 21the component of 2k in the x-y plane, then (1) becomes . e E = "5(XLX Pa). (3). Y ' The time required v to traverse a complete K “‘ orbit as in Fig. l is X dK dK ‘h 11 27F 1 ,S... dK =-£-. _-.-_ a _-._ e3 L T eB .‘a' mb dA (4) Fig. l where mbis the cyclotron frequency and dKlland dflare defined by Fig. l. The cyc- lotron mass, me, is defined by wb E eB/mcc , (5) or, using (4), m = eB = h d’cll c who 2w v (5) -11- OPEN I’ORBIT I IN (010)-PLANE I Ilfiooj-AXIS CLOSED ELECTRON AND PERIODIC OPEN ORBIT HOLE onmrs OPEN ORBIT EXTENDED ORBIT I \ % ‘5‘) «3 (d) APERIODIC OPEN ORBIT EXTENDED ORB” (taken from E. Fawcett, Ref. 25) Figure 2 Various types of closed and open orbits. IIVJ h‘ er -12- -1 1 Since vL = h d€/dKL , 2 dK 2 _ h 11 _ h dA mc I 27.jr de dKL — w de ’ (7) where dA is defined in Fig. 1. Fig. 2 shows, in an extended zone scheme, some of the types of orbits possible for a hypothetical cubic metal with a multiply-connected Fermi surface. For a general field direction, there will be no cpen trajectories and all the closed orbits will be electron orbits, i.e., they will enclose occupied regions in kfspace. Fig. 2(d) shows an extended orbit which must pass through several zones before closing back upon itself. Figs. 2(b) and (c) define periodic and gperiodic cpen orbits as shown. In Fig. 2(a) in which the field is along a symmetry axis, there are no cpen orbits but there are closed hole orbits which enclose unoccupied regions in kfspace. This is called a singular field direction for reasons to be ex- plained later in this section. Kinetic Formulation of Transport Problems Let fo(k,r)dkdr'be the equilibrium number of particles in dkdz, When electric and magnetic fields, E and g, are present, there are forces on the particles which change the distribution to rm) = roe) +s(§g) <8) -13- where g(k) is the (small) diSplacement from equilibrium; we now assume no dependence on g, Now by (8), Bfo 895,) = "5'5“ be. (9) where A6 is the average energy gained by an electron from the field E, The electrons are accelerated by E but are scattered at a rate l/T where T is a relaxation time as- sumed here to be independent of k, The effective ac- celerating field is then an“) = se““‘t"/T (10) where the exponential factor is the probability that a particle scattered at time t' will reach time t without further scattering. Thus I: e [XkIt')'Ee'(t't')/T dt' (11) -.,, t e (;%)f%(tt)-§e‘(t't')/T dt'. (12) This is the equation of Chambers. Now consider a new set MM and 8(Est) of krspace variables. The point k'can be specified by: (l) the energy 5 which, for any orbit, is constant in a magnetic field, (2) the component of k'along E, kz, also a constant, and -1h- (3) a phase variable s defined by dm = wbdt (13) ~ dK .. is __.__.11 a _ (130er v, . (14) This variable is chosen because it increases at a constant rate m =lmb in a magnetic field, and m = 2r for a com- plete circuit. We can therefore consider the 'out-of— balance' part of the distribution function, g(k) to be a function of (e,kz,m): T Bf n s(€.kz.m) -= f—(———,€° s-r(e.kz.o")e (M We as" . (15) C Then the current is e 1 . _ e l. :1 = Z? gangs — I? gjyemzmmemzewedkzdcp . (16) Substituting (15) into (16) and using 5—81?" ( > < > lim = -5 e - e , l7 T-a-O e F where EF is the Fermi energy, we obtain 27 m 2 m A n - _ 1 e - C I! n -(m-m AA” T. :1 - I113 Ff! dszmc-D: £(€F.kz:mydcp XIEFskch )9 0 (E8; -m 1 Changing variables and using i=g‘gs (19) -15- we have for the conductivity tensor in Cartesian co- ordinates, 27 w 2 m l e . c . - t “is = mpjwz 5;]! dcpdm'vi(1 28308:. 039 em 2 7m 2 Anon-333v em 2 E :25 SH Hagan-2.6 ode a wee a fin am 2 m 2 a «wee am 2 5 demo .HHH as" .s peerage-mace am. 2 m 2 ass-seas am 2 as ease-e 3. .: Em...- We. a a I c a poaemeomaooes em 2 m G Anceeaseewv em 2 was “some? :4 .H 360 :o- dado-mace o o e m noboOmwMWm-Ea Omega-Sat consummmoaBoS-meg was flame momommata a has zen . .mfimpoe e0 moaunoaose oeuocmmsocm>fimw UHOfiMIemfig mo zsmEEsm .HH manna -23- d/2 An = Zfiz. ABZ(kZ)dkz . ( - /2 \N \O V Summary of High-Field Galvanomagnetic Properties The field dependence of the galvanomagnetic pro- perties of metals in the high-field limit is summarized in Table II, taken from Fawcett's review article.(29) By magnetoresistance, we will always mean transverse magneto- resistance which we define as A B - 0 where the resistivities are measured with the field per— pendicular to the current. The longitudinal magneto- resistance has a difinition similar to (40) except that the field is parallel to the current density g. The transverse-odd field is defined as RHB/J and the trans— verse—even field is defined as RTEBe/J, where pr(B) - oxy(-B) R a (41) H 2B pr(B) + p (-B) X RTE 2B2y II‘ ° (#2) be 7" h. y\s (n In Table II, in the case of open orbits in one direction, Ap/p and RTE depend on the angle a between {,and i, where x is the direction of Open orbits. This comes about be- cause we must measure the voltages in the sample coordinate system rather than in the system in which the Open orbits are in the i direction. We therefore must make a similarity g_ transformation of'? as lg’ given by (37) with the rotation matrix corres- ponding to the rotation a shown in Fig. 4. This XV leads to the angular de- pendences shown in Table Fig. 4 II. Table II also points out the major qualitative dif- ference between the magnetoresistance behavior of com- pensated and uncompensated metals. For an uncompensated metal, the magnetoresistance tends toward saturation for 2 a general field direction and is prOportional to B only when there are Open orbits perpendicular to the field. For a compensated metal on the other hand, the magneto- resistance is prOportional to B2 for a general field dir- ection and approaches saturation only when there are Open Orbits perpendicular to the current direction. This means Iflfirt Open orbits are somewhat more difficult to find in -25- compensated metals than uncompensated ones because the sample axis (which determines the direction of g), must be chosen such that it is normal to an Open orbit dir- ection if open orbits are to be observed. In the next subsection we turn to a discussion of the criteria for the existence of compensation in metallic compounds and the information about the quantum chemistry that might be gained from a study of the state of compensation in these compounds. Rules for Compensation in Intermetallic Compounds The experimental determination of the state of com- pensation in intermetallic compounds will be useful be- cause, in general, the complexity of the chemical binding precludes a knowledge of the number of electrons in con- duction bands. However, the success or failure of the rules for compensation given below may indicate, for example, that the Fermi surface of a given intermetallic is consistent with a single OPW model or, alternatively, that some of the 'valence' electrons have gone into localized bonding orbitals. Consider a perfectly ordered intermetallic compound having 31 and s atoms of atomic number Z1 and Z2, res- 2 pectively, per unit cell. Let there be N unit cells in —26_ the crystal, F full zones, and J hole zones.(30) Since the total number of electrons must equal the total num- (31) her of occupied states, we have slz1 + $2Z2} N = 2FN + neN + (2J - nh)N. (43) Denoting the quantity in braces by nT, the total number of electrons per unit cell, (43) becomes -nA E ne - nh = nT - 2(F + J) (44) Therefore if nT is odd, the metal cannot be compensated and nA must be an odd integer. If nT is even, either nA must be an even integer or the metal can be compensated if nT = 2(F + J). However, compensation is to be expected when nT is even because of "spilling over" arguments. For all nonmagnetic metals which have been investigated, if nT is even, the metal is, in fact, compensated. If, in a metalliccompound, the core electrons lie appreciably lower in energy than the 'valence' electrons, (44) becomes = (slV + S2V2) - 2(FV + J) ’nA l (45) th where V is the'valence'of the i type of atom, FV is the 1 number of zones filled by the 'valence' electrons, and nV -27- is the total number of 'valence' electron per unit cell. Eq. (45) should be most useful when the number of atoms per unit cell is fairly small. For example, the equi— atomic ordered alloy B'- CuZn has the CsCl structure so that s1 = s2 = 1. If we assume Vbu = l and Vin = 2, then n.V = 3 so that CuZn should be an uncompensated metal. Ioreover, a suitable modification of a single ~0PW Fermi surface for this metal, which is consistent with the mea- sured dHVA periods,(32) predicts hole surfaces in the first zone, multiply—connected hole lenses in the second zone, and no overlap into higher zones. This implies F 0 v: and J = 1 so that nA = -13 this can be checked by a direct measurement of the Hall coefficient in high fields. The application of (44) and (45) to AuSn will be discussed in section 5. 3. Preparation of Samples In this section we discuss attempts to produce single crystals of several magnesium intermetallics, the preparation of AuSn, and comment upon the necessary criteria for obtaining long mean free paths in inter- metallic compounds at low temperatures. Metallurgical and Sample Analysis Techniques With minor variations, the procedure for making all of the alloys was as follows: The pure metals were etched, washed with distilled water, dried with a heat gun, and weighed in the correct proportions to about 50 micrograms on a Mettler balance. A small, high-purity graphite cru- cible was then outgassed for several hours in a Lepel induction furnace; the temperature was held above 1000°C and the pressure was kept below about 10'” mm Hg during this outgassing. The pure metals were then placed in the crucible and melted together either under vacuum (pressure 5 10-4 mm Hg) or in about one atmosphere of argon - depending upon the vapor pressures of the metals involved. In some cases the alloy was chill-cast by pOuring it into a cool copper or graphite mold several times. In other cases mixing was done by agitating the melt mechanically and by the action of the rf field. When the melt was not poured, the sample was cooled, turned over, and remelted about five times. -28- -29- Two methods of producing single crystals were used: zone refining and the Bridgman method. The zone refining methods were similar to those described by Lawson and Nielsen(33), with the heating element being either a length of Kanthal resistance wire or a small rf coil. The zone refined samples were in the form of rods of diameter about 1/8” and length about 6”. The samples were situated in a long graphite boat which, in turn, was inside an evacuated pyrex or vycor tube. The heating element was pulled along by a geared-down synchronous motor at a rate of about one inch per hour. In the Bridgman method the samples were enclosed in evacuated, sealed-off, pyrex tubes or in graphite crucibles which were inside evacuated, sealed-off, vycor tubes. The sample holder was suspended by a chromel-alumel wire and was drOpped atabout 3/4" per hour through a temperature gradient in a double furnace. The temperature of each part could be kept constant to $100; schematic diagrams of the double furnace, its wiring diagrams, and its electronic temperature control circuits are shown in Appendix A. The first attempts to prepare single crystals were made on several magnesium compounds: Mg2Cu, Mgsz, and Mng. These compounds turned out to be fairly difficult to prepare for several reasons. Magnesium has a relatively high vapor pressure at the melting temperatures of these compounds and therefore, was continually deposited out on -30- a cool part of the container. Furthermore, magnesium attacks quartz so that the Vycor tubes had to be coated with a carbon film to prevent deterioration of the tubes. This made it very difficult to tell whether or not the metal was actually molten in the graphite boat used for zone refining. In the case of MgQCu, the alloy invariably became coated with a black scum which could not be iden- tified. Several ingots of Mg2Pb were prepared by melting the two metals in about one atmOSphere of argon gas in the induction furnace. Hewever, upon exposure to the atmosphere for several hours, a shiny ingot of Mg2Pb would turn into a pile of black dust. The compound Mng which has the CsCl structure is similar to Mgng in that it also decomposes upon exposure to the atmOSphere. But by keeping the ingot in nitrogen gas or liquid nitrogen, it was possible to enclose the sample in a quartz tube and pass a molten zone through it five times. Two of these zone refined samples had resistance ratios of 125 and 94. A crude sample holder was made and the magnetoresistance of the R = 94 sample was measured as a function of magnetic field direction at a field of 21 kG. The magnetoresistance was isotropic to within experimental accuracy'(~5%) and had -a value of about 0.5. Possible reasons for this isotropy are: (l) the sample may not have been a single crystal; it was not checked by X-rays because of the decomposition problem, (2) there may be no Open orbits an/ i— in Mng, (3) the field may not have been sufficiently high that the electrons were in the high-field region. One of the interesting questions one can ask about the electronic structure of metallic compounds is: For a compound to be an OPW metal, is it an unnecessary, necessary, or sufficient condition that the constituent metals themselves be OPW-like? If the answer to this question is that it is a sufficient condition, then Mng would be an OPW metal. Since the symmetry of this metal is so simple (simple cubic), the single-OPW model was worked out. The model gives small hole 'pockets' in the first zone, a 'concave cube' hole surface in the second zone, electron 'pancakes' in the third zone, and electron 'cigars' in the fourth zone. There are no Open orbits in this model. Because of its simple crystal structure, it would be interesting to investigate the Fermi surface of Mng.with the leA.effect to see if it does, in fact, con- form to the single-OPW model. As mentioned above, the metallurgical problems as- sociated with the magnesium compounds are formidable. In particular, it is very difficult to cut a sample from a large single crystal of a reactive material, orient it with.X-rays, and mount it in a sample holder. For these reasons it was decided to change to a more tractable alloy system. 7. "/2- The gold-tin system is attractive because both of the elements have low vapor pressures and are quite non- reactive with air. The melting temperature of the com- pound AuSn is 418°c,(34) which is well within the cap- ability of the Bridgman furnace. Furthermore, AuSn has the hexagonal, NiAs type structure with c/a = 1.278; there are four atoms per unit cell in this structure which is a reasonably small number compared with the 48 atoms per unit cell of acompound like MgECu.(35) Other motives for studying AuSn are that it has been studied by a variety of tranSport(36) and magnetic(37) techniques as well as by the deA effect.(38) ' After growing the single crystals by either zone re- fining or the Bridgman method, the resistance ratios were measured as a function of length along the rods. This was done by attaching phOSphor— bronze current and potential Spring clips to the sample along its length. A current of about one amp was passed through the sample in both dir- actions and the potentials read at T = 2950K. and T = 4.2OK. Table III lists the various samples grown, their approximate dimensions, the method of preparation, the type of container, and the minimum and maximum or average resistance ratio for each sample. The samples listed are not all monocrystals; there are polycrystalline portions on many of the Bridgman samples, especially near the initially solidified end. Samples VIII-l, 2, 3 and IX-l,2 were grown in a graphite crucible having three thin slots Table III. List of AuSn crystals grown. 32;. Dimensions Method of Container Rmin/Rmaxh (in), Preparation or Rave I 1/8 x 6 ZR(6)a GBb 12 1-1 1/8 x 4 BC PTd 36/60 II 1/8 x 4 B GCe 16/35 IIIf 1/8 x 1/8 x 6 ZR(6) GB 10/42 IV 1/8 x 5 B PT 14 'V l/4 x 5 B PT 19/26 VIg 1/8 x 6 ZR(9) GB 10 VII 1/8 x 5 B PT 13 VIII-l 1/16 x 1/16 x 4 B 00 38/54 VIII-2 1/16 x 1/16 x 4 B GC 39/60 VIII-3 1/16 x 1/16 x 4 B so 34/43 IX-l 1/16 x 1/16 x 4 B so 34/166 IX-2 1/16 x 1/16 x 4 B CO 46/130 a - ZR(n) = zone refined; n passes b - GB = graphite boat c - B = Bridgman method d - PT = pyrex tube e - CC = graphite crucible f - part of sample II used as a seed crystal g - part of sample V used as a seed crystal h - R 2' p(295°K)/p(4.2°K) Table IV. List of AuSn samples. Cut from Samplea _§‘_ ._TE __§i I-l 60 7° 88° III 42 19° 16° v 25 20° 36° IX-l 73 4° 60° VIII-2 116 12° 88° a - i.e. cut from sample designated in Table III. b - m c - 9 angle between plane of [0001] and J and {10I0(. angle between [0001] and J. -34- _35- cut down to its center. In this way it was possible to grow three crystals with only one 'drOp' through the Bridgman furnace. At the suggestion of W. B. Pearson, samples VIII and IX were made slightly gold rich and this seemed to increase the resistance ratio. Sample VIII was 0.1 at.% gold rich and IX was 0.2 at.% gold rich. For reasons to be explained below, the crystals tended to have the highest purity (i.e. highest R) in the same regions in which there were a lot of small angle grain boundaries. For this reason it was necessary to take four to six X-ray photographs to find a large enough 'single' region from which to cut a sample. The X-ray technique used was the Laue back-reflection method using a molybdenum target. The film used was Kodak type KK and the exposure times were about 30 to 40 minutes. The sam- ples were cut out with a Servo-Met spark cutter. The samples on which liquid helium runs were done are listed in Table IV with their resistance ratios and orientations. In the course of orienting the hexagonal AuSn cry- stals, it became necessary to calculate the interplanar angles in order to construct a standard (0001) stero- graphic projection. These angles are a function of the c/a ratio for hexagonal crystals and have already been published for magnesium, zinc, and cadmium.(39) Because of the increasing interest in electronic and other pro- perties of hexagonal transition metals and intermetallic -36~ compounds, the crystallographic angles were calculated on the M.S.U. CDC 3600 computer for 1.10 s c/a s 1.90, in 0.01 steps.(40) These bounds were chosen because most hexagonal elements and many hexagonal intermetallic com- pounds have c/a ratios within them. If we exclude graphite, c/a ratios of the hexagonal elements vary from about 1.14 for selenium to 1.88 for cadmium.(ul) Also, for example, there are many intermediate phases of the NiAs type for which 1.2 g’c/a g 1.8.(42) The calculation is described in Ref. (40) and the results are contained in Appendix B. The Achievement of a High Degree of Order in Intermetallic Compounds. Consider the schematic, partial phase diagram of the gold-tin system in Fig. 5.(43) AuSn is a compound which, in principle, is simple to prepare because if one solid- ifies a melt which is slightly off the correct stoichio- metry, the solid formed will have the exact stoichio- metry over at least part of the solid. For example, if one cools an alloy at the point B on Fig. 5, the compound of perfect stoichiometry will begin to solidify out at point C. The residual melt will then slide down the liquidus toward the right until point F is reached. Then the compound AuSn2 will begin to precipitate out. If one solidifies a long thin rod of nominal composition Au Sn 1 1 from the bottom up, it is indeed found that the bottom end -37... Temp 0C 50.0 66 Atomic Percent Tin Figure 5 Partial phase diagram of AuSn system. -38- Temp 0C I I I I I I I I J 49.8 50.00 50.2 Atomic Percent B Figure 6 Phase diagram of non-ideal intermetallic compound AlBl. —99_ has a more nearly perfect stoichiometry. That is, the bottom end has a much higher resistance ratio than the top end (See Table III, samples VIII and IX). Unfor- tunately, the bottom end also tends to be polycrystalline and/or to have many small angle grain boundaries because, in the growth process, one of the crystals has not yet had a chance to dominate over all the other crystals which have started to grow. The preparation of a peritectic compound such as AuSn2 would be rather difficult. Cooling a melt at point D would result first in the solidification of AuSn at E. Only when the melt had reached the composition at F would AuSn begin to solidify at point G. 2 The preparation of high purity compounds of the type we have called 'simple' is, in fact, more complicated than the elementary discussion we have given above. The reason is that the vertical line representing the solidus of an intermetallic compound on a phase diagram is not, in gen- eral, of infinitesimal width. Compounds can exist as substitutional or subtractional (vacancy) solid solutions between certain limits of homogeneity as shown in Fig. 6. For example, the separation of the limits of homogeneity is 0.5 atomic per cent for AuSn(44) and 2.7 atomic per cent for MgCu2gu5) What magnitude of resistance ratio would one expect for a compound having a phase diagram like Fig. 6? If we denote the compound by A50ixB50 x’ then from Fig. 6, 3F ~40— a rough estimate of an average value of x might be ~x0.1. This corresponds to about one imperfection in 103 atoms. From a consideration of the purities of pure metals and their resistance ratios, one can induce the following order- of—magnitude relation between resistance ratio, R, and the amount of impurities, I, in parts per million present. R ~ 104/1 , 1315.104. (46) That is, four-nines (i.e. 99.99 at.% pure), five-nines, and six-nines pure metals typically have resistance ratios of about 102, 103, 104, respectively. If we assume that the same approximate rule holds for intermetallics, we could expect the compound in the above example to have R -.10, Fig. 7 is a plot of (46). The points on the graph were taken from a table of R versus composition in Jan et.al. and it is seen that AuSn does qualitatively follow (46). From Fig. 7 and Table III, it follows that the purest part of sample VIII (R.~'l50) was within about 60 ppm of exact stoichiometric prOportions. This is a rather remarkable degree of crystalline perfection for binary ordered alloy- a much higher degree of perfection than can be achieved in metallic superstructures of the CuBAu or CuAu type.(47) In this discussion we have neglected as being small, the residual resistivity due to impurities in the original pure gold and tin; the gold used was five-nines ASARCO and the Resistance Ratio R -41- 10 Figure 7 J 10 2 103 10 Impurity Content, I, in ppm Graph of resistance ratio vs. impurity content for metals. -42- tin used was six-nines COMINCO. The process of lowering a sample through the Bridg- man furnace to make a single crystal typically took about fifteen hours. For the zone refined samples, each pass took about four to six hours so that several days were spent zone refining a single sample. Thus, with the pre- liminary weighing, etching, outgassing, sealing off, etc., it normally took three or four days to prepare a single crystal with the Bridgman method and about a week to do so by zone refining. The determination of resistance ratios, checking crystals for singleness, cutting to size, and final orientation took at least a week for each sample. It can therefore be seen that an appreciable amount of the time Spent in this research was devoted to sample prepar- ation. Summarizing, we have tried to show in this section that as regards the preparation of highly ordered metallic compounds, the best chances for success lie with those compounds having the following properties: (1) the sep- aration between the limits of homogeneity of the inter- mediate phase should be extremely small, and (2) the intermediate phase should occur at an exact stoichiometric composition. 4. Apparatus and Experimental Technique The experiment consists of measuring the magneto- resistance and Hall coefficient as a function of the magnitude and direction of the magnetic field. Fig. 8 shows a schematic diagram of the apparatus and circuits used to measure Ap/p as a function of B. The sample, imInersed in liquid helium at 4.2°K, is held in a fixed position in the field of a Magnion superconducting solenoid having an inner diameter of 1.5" and a maximum field of about 58 kG. The source of the sample current was several large lead storage cells producing a current that was held constant to one part in 104. A fairly large sample current of about three amperes was used in order to obtain transverse voltages of a readable mag— nitude, i.e., of the order of microvolts. The small DC voltages were amplified with a Keithley model 149 millimicrovoltmeter which fed the YAaxis of a Moseley 2D, X-Y’recorder. The noise level of this arrangement was about 5 x 10"8 volts. For the function-of—field runs illustrated in Fig. 8, the X-axis diSplacement was pro- portional to the current (and therefore, to the field) in the solenoid. Fig. 9 shows the sample size and shape as well as the points of contact.of the potential probes. Only five of the probes, e.g. l-5, were actually necessary to com— pletely determine the vector electric field, E, in the -43- —44— Figure 8 Schematic Diagram of Apparatus and Circuitry 10 I. I— I —> r—fl ’ Keithley MOSELEY Amplifier -——Y X-Y RECORDER (L__. __ r' ‘7' '- ‘" — r — ‘1 I X I \S \ I I , SOLENOID l POWER | SUPPLY I L I L— — —- —— —-- --I Superconducting Solenoid «yli‘l'; Z Liquid He Bath 8 . I3 .. k J_ a ”It 5 H‘s... IE_ 7 Figure 9 Diagram Showing Sample Size, , to 1+ ‘2‘" Shape, and Potential Probe 0'5 ' \6 o Placement 3 -45- " Drive Shaft Aluminum _ Spiral Gear ,Support, Hollow Cylinder Probe Springs Teflon Spacer Teflon Busmng ' I—l/2"Cublc Lucrre Sample Holder Figure 10 Sample helder and rotating apparatus. -46- sample; the three extra ones were included as a safety factor against open circuits; as shown in Fig. 10, the thin brass voltage probes were held against the sample with metal springs and it was not known before the ap- paratus was actually tested at liquid helium temperatures, how reliable the contacts would be. In practice, the probe spring method was wholly reliable: not one open circuit was encountered in any of the runs. In order to measure the galvanomagnetic prOperties as a function of magnetic field direction, it is nec- essary to rotate the sample in the longitudinal field of the solenoid. Fig. 10 shows an exploded view of the apparatus used to do this. The lucite sample holder in Fig. 10 was designed so that the sample could be mounted for transverse or longitudina1-to-transverse runs. In the transverse runs glwas always perpendicular to B,as illustrated in Fig. 10; in the longitudinal-to-transverse runs, the sample could be rotated from a position where J,was parallel to B,to a position where J,was perpendicular to B, The spiral gear arrangement is similar to that used by Thorsen and Berlincourt.(u8) for pulsed field dHVA ex- periments. The drive shaft, which emerges from the tOp of the cryostat through a "quick-coupling" vacuum seal, is coupled to a linear potentiometer through which a constant current flows. The voltage taken from this -117- potentiometer, which is proportional to the angle of rotation of the sample, is fed into the X-axis of the X-Y recorder for the 'rotation' plots. One complete rotation of the drive shaft corresponds to a rotation of the sample of 4.50. The misorientation due to back- lash in the gears is estimated to be less than 1°. In- cluding the error in the X-ray orientation of the samples, the total uncertainty in orientation is estimated to be i2°. In certain cases, where the passage of B,through a symmetry plane of the crystal corresponds to an extremum in the rotation plot, the uncertainty in orientation is considerably smaller than 2°. The rotation plots were always made with the solenoid in the persistent current mode. The rotation and function- of-field data were taken point-by-point using the point plotting attachment of the X-Y recorder. Current leads of No. 34 cOpper wire were soldered onto the sample with In-Bi eutectic solder (22 at.% B1, superconducting at 4.2°K(u9), melting temperature 72°C.) The current leads were brought to the sample through a hole on the axis of the left side of gear shown in Fig. 10. Small No. 42 cOpper wires were soldered to the 0.014", sharpened brass voltage probes. These wires were glued to the lucite block with a general cement and brought out a hole on the right side of the cylinder shown in Fig. 10. The flexibility of the current and potential leads per- mitted the sample to be rotated through 180° without difficulty. -48- About ten liters of liquid helium was needed to pre- cool the solenoid because of its large heat capacity; it weighs about fifteen pounds. It was found that the best way to precool the solenoid to liquid nitrogen temperatures (770K) was to dip it into a dewar of liquid nitrogen for one hour. It was then quickly withdrawn from the liquid nitrogen bath and lowered into a stainless steel, double- dewar. Immediately thereafter, the liquid helium transfer was begun. The most efficient transfer pressure was ~5/8 pounds until the solenoid was completely immersed and ~3/4 pounds thereafter. The level of the liquid helium in the dewar was monitored by four carbon resistors placed at various heights above the bottom of the dewar. Each car- bon resistor formed one arm of a resistance bridge which was balanced when the resistor was immersed in liquid helium. Each resistor was surrounded with styrofoam to keep the cold helium gas from lowering its temperature to 4.2OK before it was actually covered with liquid helium. In this way, a sudden drOp from almost full scale to zero was noticed on a microammeter when a given resistor became immersed. In order to achieve fields above about 40 kG, it was necessary to "train" the solenoid by quenching it once or twice. By quenching is meant the sudden transition of the superconducting solenoid from the superconducting to the normal state with a moderate or high current flowing in it. It was also necessary to retrain the solenoid upon -2). 9- changing the direction of current in it. The occurrence of these quenches was unfortunate because about a liter of liquid helium was evaporated for each quench and a) considerable amount of time was wasted bringing the field back up to a high value. The field could not be taken from zero to a high value arbitrarily fast; it was necessary to monitor the inductive back-emf across the solenoid, vL = L dIS/dt, and to keep v < 1 volt for L B 3'40 kG and Vi 5,50 millivolts for B > 40 kG. This meant that it took about one-half hour to change B from 0 to 40 k0 and about 1.5 hours to change B from 40 kG to 56 kG. If the above limits on.Vi were exceeded, a quench of the solenoid would result. Even if'V was L kept within the above limits, the solenoid would quench until it had been trained as explained above. Also with reSpect to the performance of the solenoid, during one run, the liquid helium bath was pumped on to lower its temperature to about 1.30K. This was done to look for de Haas - Schubnikov oscillations in the magneto- resistance. Unfortunately, however, because of the re- duced temperature, the solenoid became very quench prone even though it had already been trained at 4.20K. This degradation effect has been observed before and although the phenomenon is apparently not completely understood, it seems to be connected with the effect of temperature on the (50) flux-jumping mechanism. S50.- As explained in Appendix C, it was necessary to change the direction of the field in the solenoid to determine the Hall voltages. Let the magnetoresistance Ap/p and the pair of orthogonal transverse voltages‘V£ be considered functions of B and t where B > O (B < 0) refers to the up (down) direction of field and t is the angle of rotation of the sample. Let Ii be angles at which there are dips or peaks in the rotation plots. Then, in a typical run, the following quantities were measured in the order given: (1) 09/9 (440 kG, I). (2) vt(+40 kG, l). (3) Mo (+50 kG. I). (4) Vt(+5° kG. I). (5) Ap/p (B > 0.1),). (6) Mo (B < 0. I2),t0 -40 kG. (7) vt(-4o kG. I). (8) Ap/o (B < 0. I2)ito -50 kG. (9) vt(-50 kG, I). (10) Ap/p or vt as functions of field at other interesting angles Ii until the helium ran out. The run described above is an ideal one; the function-of-field plots were sometimes interrupted by the quenches previously referred to. Since the topological prOperties of the Fermi surface determine only the field dependence of the galvanomagnetic properties and not their absolute values, the solenoid was not accurately calibrated. The magnetic conversion ratio, MCR = 2.43 kG/Amp, was determined by the manufacturer to an estimated accuracy of 10%. 5. Results and Discussion The Crystal Structure of AuSn Fig. 11 shows the hexagonal, NiAs structure of AuSn. The black balls representing the gold atoms are on a simple hexagonal lattice and the white balls representing the tin atoms are on a hexagonal close-packed lattice. The space group. P63/mmc, indicates that there is a six-fold screw axis and also a glide plane along the hexagonal axis. Fig. 12 illustrates the primitive translation vectors, a1, a2, E3’ 2; in the direct lattice and the primitive translation vectors, 21’ be, 25, in the reciprocal lattice. Fig. 13 shows a partial (0001) standard stereographic pro- jection(51) for hexagonal crystals. Both figures show that all of the §,directions are normal to {1120} planes and the 1; directions are normal to {101:0} planes. Similarly, the a vectors are along (1120) directions and the b vectors are along <1OIO> directions. On Fig. 13 and on all succeeding stereograms, the <1I20> directions are marked as dots and the <10I0> directions are marked as slashes on the peri- meters of the stereogram. Magnetoresistance and Hall Effect Fig. 14 shows the magnetoresistance as a function of magnetic field direction at 50 kG, for AuSn I. This sample had a resistance ratio of 60. The current direction, given -51- 2N; no\o n!_.m\N.M\_3 - cm 5. Aux-3036.3” =4 ass-Xe.- H5010 84mm -53.. (1120) (1010) [1120] [1210] [0110] Figure 12 Direct and reciprocal lattices for hexagonal crystals. 1120 E53 0001 cab,3 'I2IO 22 0110 9.2 2110 1010 al “’ b ~l Figure 13 Partial standard (0001) stereographic projection for hexagonal crystals. -5h- Au Sn I B=50kO 1.5— O b :0— sale Q. <3 0.5— J-' ° " (l0l0) 0.05—I-r—Lr—J—r l lw—l—r—I—u— 90 -60 —30 0 so 60 90 MAGNETIC FIELD DIREC TION Figure 14 for AuSn I. Graph of Ap/p vs. magnetic field direction -55... by the cross on the stereogram, is 20 away from the basal plane and 70 away from a.{1OIO} plane. The tOp rotation curve is a transverse run and the bottom one is a nearly longitudinal-to-transverse run. Both curves are essentially symmetrical about point b, i.e., they do not cross at this point. The small letters on the curves and stereogram per- mit making a one-to-one correSpondence between the field directions on the great circles on the stereogram and the field directions on the rotation curves. Although the curves were made in a point-by-point manner, for simplicity of pre- sentation, no experimental points are shown on Fig. 14 or other rotation plots. The data were taken quasi-continuously, i.e., often at one or two degree intervals. Each point was taken with the solenoid in the persistent current mode and with the sample motionless. Consequently, the noise due to emfs induced by varying flux through the measuring circuit was negligible; the total noise was only of the order of the thickness of the line in Fig. 14. Let‘V1(B) be the voltage measured along the length of the sample at a field B. Fig. 15 shows a linear plot of AV 2 V1(B) - v1(0) = V1(O)Ap/p as a function of field for two different field directions on two different samples, AuSn I and AuSn IX. The figure demonstrates the closest approach to saturation and to quadratic behavior achieved with the samples used in this research. The magnetoresistance is henceforth assumed to be prOportional to Bm and the values in [AV AV O 0 AV = V1(B) - V1(0) = V1(0)AQ/€ vs. B. AuSn IX curve a, Fig. 0 0 O G O O O 0 AuSn CUPVG 90 G 0 GO 0 O 1 Field in kG o 18 0 O o O o o I d, Fig. 16 ea coco 0000000 30___ 25‘...- 20... l5.__ h)___ 5... 001;} ° Figure 15. saturating and 25 quadratic behavior 5f Graph showing approach of magnetoresistance to 2.0 .. Au Sn I a, I.3 b, L0 L0— 08 r- °'°'° § L a \ e _ o. 4 d,a O 0.2— .I I I 500 I000 5000 BR KILOGAUSS Figure 16 Log-log plot of Ao/p vs. BR for AuSn I. -58- of m are determined by log-log plots of Ap/p versus BR. (-R = resistance ratio - see pg. 2) Ap/p is customarily plotted as a function of BR so that, assuming Kohler's rule<52) is valid, samples of different resistance ratios and there- fore different purities can be compared at the same effective field. That is, the important quantity with respect to the high-field galvanomagnetic prOperties is the value of wbr = uB a BR, and not the value of the field alone. Fig. 16 is a log;log plot of Ap/p versus BR for AuSn I. The field direction for the four curves are those marked of Fig. 14. The numbers at the right of the letters are the values of the exponent m at the highest field of the curves, 56 kG. The almost complete saturation of Ap/p when B’is nearly parallel to J (curve d), indicates that the electrons are largely in the high field region. This follows from the theory in section 2; the resistivity tensor element 922 is always independent of field ig_the high field limit. Fig. 17 is a graph of the magnetoresistance versus magnetic field direction for AuSn IX, a sample for which J was 20 away from the basal plane and 120 away from a (1010} plane. This sample had a higher resistance ratio (116) than AuSn I. This is reflected in the higher maximum value of Ap/p (~4) and in the sharpness of the peaks and dips of the rotation plot. The field dependence of the magnetoresistance at the three points marked on Fig. 17 is shown on a log-log plot in Fig. 18. -59.... 4.0— a .. AuSn IX §I§ a: 50 HE G 9. 2.0... c 1.0-— Q 0 <"I°2IoTo> I I I I -90 -60 ~30 0 30 60 90 MAGNETIC FIELD DIRECTION Fngtre 17 Graph of Ap/p vs. magnetic field direction for AuSn IX. -6 O... 2!£)-’ (3.2!r- (DJ AuSn II b, l.I III 1 11 Figure 18 '0 BR KILOGAUSS Log-log plot of Ap/p vs. BR for AuSn IX. IC) -61- Referring to Table II, the summary of galvanomagnetic properties, it is seen that for a compensated metal (ne = nh), for a general field direction, Ap/p « B2 (case 11 of the table). Except for the fairly rare occurrence of cases IV and V of Table II, Ap/p saturates for a compensated metal only when there are cpen orbits in one direction and a e:F/2 (case III). Since the magnetoresistance of AuSn never tends toward saturation except when B,lies in a symmetry plane of the crystal, we conclude that it is compensated metal. The fact that the maximum value of the exponent m in Fig. 18 at point a is 1.6 rather than the 2.0 expected from theory pro- bably means that a small fraction of the electrons are not yet in the high field region at 56 kG. The fraction must be a fairly small one or the nonvanishing of Ox in (30) will y cause the metal to behave like an uncompensated one. For example, consider a compensated metal having two groups of carriers with mobilities differing by an order of magnitude. Suppose that the electrons and holes had mobility ”e and uh, reSpectively. Let ”e = 50 uh. Suppose the magnitude of B has a value such that ueB = 5 so that uhB = 0.1. At this value of field therefore, the electrons will be marginally in the high-field region but the holes will be far from it. In this case, although ne = nh in Oxy in equations (30) and (31), in effect nh is zero as far as the high-field galvano- magnetic properties are concerned. In the example cited, one would expect the galvanomagnetic behavior to be rather more like an uncompensated metal than a compensated one. -62- These kind of arguments explain why, for a transition metal like Pd which has s and low mobility d electrons, one must have very pure samples (R ~'2000) and go to fields of order 100 kG to observe high-field galvanomagnetic effects. Because of the difficulty of preparing very pure samples of many elemental metals, the galvanomagnetic properties of some of them have deviated slightly from the ideal m = 2.0 and m = 0.0 behavior expected from the theory. In practice, the behavior of a compensated metal is recognized by the conditions Ap/p > 1 and l < m 3,2 for a general field dir- ection whereas for a compensated metal, Ap/D «'1 and 0 < m < l for a general field direction.(52) Compensated metals other than AuSn for which m is appreciably less than 2.0 are Mo, Re, Pt, Fe, and Pd for which m ~a1.8(53) and Be for which m ~v1.6.(54) At point c in Figs. 17 and 18, where B,is in the basal plane, Ap/p tends toward saturation with m = 0.6. Similar behavior is observed in Fig. 16 at point 0 when B,is in the basal plane. This indicates that there are gpen orbits along [0001]; i.e., the saturation is caused by case III behavior (Table II) with a a:fl/2. At point b on Fig. 17, there is a relatively sharp dip. The field at this point is nearly parallel to [0001] and the exponent m is 1.1. At a similar orientation of B'in Fig. 14, m = 1.0. We return to this point later. _53- A reference to Table II shows that the Hall coefficient can give useful information about'Ve and Vh, the electron and hole volumes of the Fermi surface. However, we have inferred from the magnetoresistance behavior that Vé = Vh; Table II shows that Vé - Vh cannot be measured directly for a compensated metal from the Hall effect. The utility of the Hall effect is therefore somewhat less in compensated metals than in uncompensated ones. Nevertheless, Fig. 19 shows a plot of the magnitude of the Hall voltage versus magnetic field direction for AuSn IX. 0° on the plot cor- responds to B nearly parallel to [0001] and 190° corresponds to B, in the basal plane (see stereogram in Fig. 17). The sign of the Hall coefficient is negative. The magnitude of the Hall voltage at the central peak when B_is parallel to [0001] is used later in this section. Fig. 19 also shows a rather broad maximum at i90° where B_passes through the basal plane. No attempt has been made to analyse the behavior of the transverse-even coefficient, RTE‘ For an uncompensated metal, the transverse-even voltages can be used with the longitudinal voltages to give the direction of Open orbits directly.(5°) Essentially, one measures the components of the electric field along the directions of an Open orbit by measuring the B2 part of this field on three orthogonal pairs of voltage probes. For a compensated metal, however, it is difficult to -51- .XH case new compoonwe UHOfim oesosmas .m> omupfio> fifimm ma onsmfim column-o 0.0-h. o Focmmz om+ o . on: o o, AOAV _ _ _ AM_HH D. wo-nvv "mm “H A o AVNHH e ,o a m human A n¥¢ MH cm3< -65- separate the effects of the B2 voltage due to case ll be- havior from the case III Open orbit B2 voltage (Table II). The transverse voltages can be used to yield confirmatory evidence for Open orbits if one has a large amount of data on crystals of the same purity and different orientations.(57) AuSn'V, having a resistance ratio of 25, was the lowest purity sample on which a liquid helium run was done. The magnitude of the magnetoresistance for this sample was only about 0.7 at 50 kG. A rotation plot of Ap/p showed very little anisotropy with the exponent m having the value of about one everywhere. Undoubtedly, this behavior is caused by an in- sufficiently high value of th' A very crude estimate of the value of wbr can be made for a compensated.meta1 using the (58) formula from the two-band model with ne = nh, 9%- = ueBuh . If ”e is assumed to be equal to uh, then if Ap/p 2.: 1, ch a: 1. Therefore, with this crude model, mbr < l for AuSn V. Actually, we know that th 2.1 for at least some of the (low mass) elec- trons in AuSn'V at 50 kG, because dHyA oscillations have been observed at 60 k0 with samples having a resistance ratio as low as l3.(59) Fig. 20 shows the current and field directions for the two samples AuSn III and AuSn VIII. The magnetoresistance as a function of magnetic field direction for these two samples is shown in Fig. 21. The field directions labelled in Fig. 21 -66- ‘1‘ EVIII H\X :IVIII'” “'1 y (0110) < 1120> <1010> Figure 20 Stereogram showing current and field directions for AuSn III and AuSn VIII. AuSn III 39°{l6 from [000:] 3° from {I I20} I if I u, {tom} {”20} {IOTOI p. E B=SOkG :3 E AuSnllX a: -’ 60° from [000:] a J I 4" mm {IOTO} (I ‘1 3F. 1 HI l (0000 {IO 0} (0000 MAGNFTIC FIEL D DIRECTION (the zero level of magnetoresistance is not shown) Figure 21 Graph of Ap/p vs. magnetic field direction for AuSn III and AuSn VIII. -68- are planes in which the field lies as it moves along the great circles of Fig. 20. The resistance ratio of AuSn III was 42. As in the case of AuSn V, the anisotropy of the field dependence of AO/p . was not sufficiently great to relate it to topological pro- perties of the Fermi surface. The field dependence of the magnetoresistance was m g 1.4 for B S. 30 kG and m -v-1.1 for B a-56 kG. AuSn III was the highest purity sample grown that had an orientation approaching the hexagonal axis. The rotation plot, Fig. 21(a), roughly shows the six-fold sym- metry of the crystal about the [0001] axis, but the aniso- tropy of Ap/p is only about 10% of the total magnetoresistance. Fig. 21(b) is a rotation plot of the magnetoresistance for AuSn VIII, a sample having a resistance ratio of 73. pg is 60° away from [0001] and 4° away from the (0110) plane. There is a fairly sharp dip in the center of the curve which corrBSponds to the field lying in the (OIIO) plane. The 1.4 field dependence changes from B at the peaks of Fig. 21(b) to B1.0 at the dip in the center. This suggests that there are Open orbits along the [OIIO] direction and hence along all (1010) directions. The cause of the dip would be the angular dependence of case III, Table II where a = 86° 3: r/2. A possible reason why the magnetoresistance does not saturate more strongly than m = l is that the Open orbits along <10I0> are caused by a small ratio of D to A, where D is the area of -59- the Fermi surface traversed by open orbits and A is the total area of the Fermi surface. The magnetoresistance for a = m/2 then saturates at a large value A/D only when uOB >> A/D, where “o is the mobility of the open orbit electrons.(°°) If this is the correct eXplanation, then the present measurements are in an intermediate range where uOB ~IA/D and complete saturation should be achieved by employing higher fields or purer samples to increase the mobilities. Another possible explanation is that the Open orbits are caused by magnetic breakdown.(°1) Then the ratio D/A can be regarded as a function of B, starting from zero at low fields and increasing to a critical field Bb’ at which.magnetic break- down is complete. Bb is given by(62) MD'beF = (A6 )2 3 where As is the energy gap where the magnetic breakdown occurs, andlmb = eBb/mcc is the cyclotron frequency in the field Bb of the carriers of mass mo in the orbits which break down. Ac- cording to this explanation the present measurements are in the region where breakdown is only partially complete, i.e., E5 a: 100 kG. TOpology of the Open Sheet of Fermi Surface of AuSn We next summarize the results obtained from high-field galvanomagnetic measurements and use these results to construct a tOpological model for a multiply-connected sheet of the Fermi -70- surface of AuSn. l. AuSn is a compensated metal: Ve = Vh' 2. There exist Open orbits along [0001]. 3. There may be Open orbits along (1010) directions. 4. When §_is parallel to [0001], there is a tendency for Ap/p to saturate with.m.=:l.0. We discuss these points in turn. 1. That AuSn is compen- sated is consistent with the first of the rules for com- pensation given in section 2. Since s1 = 82 = 2 for AuSn, compensation would be expected from (44) and the discussion following it. Further, if we assume valences of one and four for gold and tin, respectively, then compensation in AuSn is consistent with (45) since nv = 10. 2. The nature of the rotation curves, Figs. 14, 17, 19, suggests that the band of cpen orbits along the hexagonal axis may be fairly wide; the dips or peaks as B’passes through the basal plane begin when §,is as much as ~20° away from the basal plane. We are thus led to pose the following model of Fermi surface for AuSn: the Open sheet consists of fairly large undulating cylinders having their axes along [0001]. 3. and 4. As discussed above, the relatively sharp dip in Fig. 21(b) suggests that there are Open orbits along <10I0) directions. Suppose that there were small cylinders whose axes were along <10I0) directions. These small cylinders explain both point 3. and also point 4. above. The <10I0) cylinders would make the [0001] axis a singular field direction and the magnetoresistance -71- / (1120) , ---t- <10IO> Figure 22 TOpological model for the Open sheet of Fermi surface for AuSn (not to scale). -72- would approach saturation because of case V (Table 11) be- havior. Fig. 22 shows a topological model of the Fermi sur- face of AuSn which is consistent with the above observations. Essentially, the model consists of large undulating cylinders directed along [0001] which are connected at their"bu1ges" by small cylinders along <1010> directions. It is to be em- phasized that only the toEology of this figure is significant. Since‘Ve = Vh, there exists another piece or pieces of Fermi surface having character Opposite to that of the Open sheet. Because the normal to most of the surface area of this sheet lies in the basal plane, one would expect AuSn to have a high resistivity along the 2 axis and this is indeed found to be the case; pc/pa 2: 1.5(63) where pc and pa are resistivities measured along the g’and g'axes, reSpectively. An estimate of the diameter d of the <10I0> cylinders can be made as follows. Let B,be along the singular field axis, [0001]. It is seen from Fig. 22 that for this field direction there are no open orbits. Appendix D shows that the sign of the Hall effect at a singular field direction is given by the character of the simply connected sheet or sheets of the Fermi surface. Since the Hall coefficient is negative when B,is parallel to [0001], the Open sheet of AuSn in Fig. 22 is a hole sheet. Appendix D also shows how to compute the <10I0) neck diameter d for a model similar to Fig. 22. The result is that the volume measured by the Hall -73- coefficient is V = A BZ d ’ where ABZ is the hexagonal cross sectional area of the Brillouin Zone normal to [0001]. Us1ng the Hall voltage at the peak of Fig. 19, d is calculated to be O.35(2wb3). Assuming that the cylinders have circular cross sections, the area of the cylinders calculation from the above value of d, Ad, is 0.12 A'2. This area could also be measured directly by the dHyA effect if the field were along a (1010) direction. The deA areas have been measured by Jan gt,gl,(°4) but only for the [0001] and <1120> directions. If we assume the <10I0> cylinders are sufficiently long, the area of the neck A can be computed from A<1l20)’ the dHyA area measured when p is along <1120>. Since [1010] and [1120] are 30° apart, A = cos30 A<1120) . Using this formula, one of the dHVA 0 periods A, gives A = 0.13 A‘2 which is fairly close to the area determined from the Hall effect. However, this does not prove that there are necks like the ones shown in Fig. 22; the period used to obtain the above area could have come from a completely different piece of Fermi surface. One of the interesting tranSport properties of AuSn is its thermoelectric power, (TEP). Jan and Pearson(°5) have measured the TEP of single crystals of AuSn as a function of crystal orientation. They found that there is a large positive -74- phonon-drag peak when the sample axis is along (1120) dir- ection but essentially no phonon-drag peak when the axis is along the [0001] direction. From this observation and the anisotrOpy in the resistivity, pc/pa'2:1.5, Jan and Pearson speculated that the Fermi surface consisted of undulating cylinders along the g'axis. This would give a large umklapp contribution to electron-phonon scattering in the basal plane but very little contribution in the 2 direction. The Fermi surface of AuSn appears to be relatively complicated. We have found that there are at least two pieces of Fermi sur- face and three dHyA periods were observed for each of the two field directions mentioned earlier. In View of this fact, the ideas of Jan and Pearson can only be regarded as highly Speculative; the electron-phonon interaction is very incompletely understood at present, even for the metals with (66) simple, well-known Fermi surfaces. 0n the Electronic Structure of AuSn As mentioned in the Introduction, it is difficult to predict the number of electrons in conduction bands in inter- metallic compounds. We have seen that AuSn is compensated which is consistent with nV = 10. The single-OPW model of the Fermi surface with nV = 10 was constructed using the Harrison method.(°7) Because nV is so large, the model is quite complicated; there are electrons in zones 3 through 8. -75- Further, no meaningful correlation could be made between the areas of the model and the measured dHyA areas. Since there is a screw axis and glide planes in the AuSn structure, the energy bands may stick together on certain points of the Brillouin zone faces.(°°) This complication may mean that a double-zone scheme should be used rather than the single» zone scheme. In order to rigorously determine where the bands stick together on the B2 faces, it would be necessary to determine the dimensionality of the group of the wave- vector £82 at the various BZ points.‘°9) In addition, the effect of Spin-orbit coupling should be considered to deter- mine degeneracies. Since the OPW model, at least in its simplest form and ignoring the complications mentioned above, does not seem to agree with experiment, we consider an alternative approach to the electronic structure of AuSn, that of Pauling.(7°) By considering the saturation magnetic moment of transition metals and their alloys as a function of atomic number, Pauling arrives at a value of 5.56 for the valence of c0pper, silver, and gold, where valence here means shared electron pairs (covalent bond) plus metallic orbitals (conduction electrons). The valences of elements to the right of cOpper are 4.56 for zinc, 3.56 for gallium, 2.56 for germanium, and 1.56 for arsenic. The same valences are assumed for elements below each of the above listed ones. In Pauling's theory, for a substance to be a metal, there must be 0.72 metallic orbitals per atom. The -76— metallic orbital permits the unsynchronized resonance of electron pair bonds from one interatomic position to another by the jump of an electron from one atom to an adjacent atom and this leads to stabilization of the metal by resonance energy, and to the electrical prOperties of metals.(7l) We simply quote from Pauling's book his explanation of the structure of AuSn in terms of the valence electrons of gold and tin:(72) "Each tin atom*~ is surrounded by six gold atoms at the corners of a trigonal prism, with the distance Au-Sn = 2.847 A, and each gold atom is surrounded by six tin atoms at the corners of a flattened octahedron, and also by two gold atoms, at 2.756 A, in the Opposed directions through the centers of the two large faces of the octahedron. The tin atoms are arranged in the positions corresponding to hexagonal closest packing, but the axial ratio c/a has the value 1.278 instead of the normal value 1.633. We predict for gold the valence 5.56, and for tin either the metallic valence 2.56 or the covalence 4. The Au-Sn distance is much too small to correspond to valence 2.56 for tin, but it agrees well with the valence 4. With this valence the Au-Sn bonds have bond numbers 2/3, [bond number equals the ratio of valence electrons per atom to number of bonds], and the interatomic distance predicted with use of the si ale-bond radii 1.338 A for gold and 1.399 A for tin is 2.8 3 A, in almost exact agreement with the experimental value 2,847 A. Accordingly the tin atom is quadrivalent, without a metallic orbital, and its four valence bonds resonate among the six positions connecting it with the ligated gold atoms. These bonds use up 4 of the total of 5.56 valences of gold. If the axial ratio of the crystal had the value 1.633, the remaining 1.56 valences of gold would not be utilized; however, by compression along the c axis, keeping the Au-Sn distance constant, the gold atoms that succeed one another along the c axis can be brought into a suitably small distance from one another to permit Au-Au bonds to be formed. The bond number predicted for these bonds is 0.78, and the Au-Au distance that is pre- dicted is 2.741 A, in close approximation to the observed distance 2.756 A. The system of metallic valences and radii accordingly provides an explanation of the interatomic dis- tances, including the compression along the hexagonal axis to give the abnormally small axial ratio." -77... If the 1.56 valences per atom of gold which are in the Au-Au bonds are regarded as weak bonds, in comparison to the Au-Sn bonds, then one might expect about 3 conduction electrons per unit cell for AuSn. This is in contradiction to the 10 con- duction electrons per unit cell used in the single-OPW model of the Fermi surface. If, in the future, the geometry of all portions of the Fermi surface of AuSn becometwell-known, it will be interesting to see if the ideas of Pauling bear any relation to the actual number of electrons per unit cell in Conduction bands. Another result; bearing on this question is the existence of superconductivity in AuSn.(73) The tran- sition temperature is 1.25°K. According to Matthias,(74) a necessary condition for the occurrence of superconductivity in compounds and alloys above 0.1°K appears to be that the average number of valence electrons per atom cannot be smaller than two or larger than eight. If, as in Pauling's theory of AuSn, we regard the electrons in two tin atoms per unit cell as simply forming localized bonds with some of the valence electrons of gold, then AuSn would have an average of 1.5 valence electrons per atom. The existence of superconductivity in AuSn is therefore in disagreement with Pauling's theory. Again, an accurate determination of the Fermi surface geometry would settle this question. 6. Conclusions The results we have described represent the first observations of high-field galvanomagnetic effects in inter- metallic compounds. We have shown that these effects can be observed in these metals with resistance ratios of the order of 100 and fields of the order of 100 kG. The open orbits observed in AuSn have been used to construct a tOpological model for the Open sheet of Fermi surface in this metal. We have implicitly stated that the interpretation of high-field galvanomagnetic properties is considerably aided if there are data on a large number of high purity, accurately aligned samples available. Therefore, good metallurgical equipment and techniques for accurately seeding and zone- refining samples are needed unless, of course, the samples can be obtained from other sources. It can be argued that the necessity to use such high fields is a disadvantage because it is likely that magnetic breakdown will occur causing open orbits to appear which are not normally present on the Fermi surface. Hewever, cpen orbits due to magnetic breakdown can be identified because samples of differing purity will not obey Kohler's rule if magnetic breakdown is present.(7°) Again, this would neces- sitate very accurate control of sample orientation and purity. It is obvious that an investigation of a given inter- metallic by both the high-field galvanomagnetic effects and the deA effect would yield much more information than by -78- -79- either of the techniques alone. As stated on p. l, the interpretation of dHyA data is very difficult for compli- cated metals, except if one has a relatively good model to guide the interpretation. Finally, we have seen that there have been two main approaches to understanding the properties of intermetallic compounds, valence bond theory and band theory. As we have discussed for the case of AuSn, the valence bond theory is based on the concepts of bond directivity, resonating bonds, bond lengths, etc. In band theory, however, crystals tend to assume a structure such that certain Jones zones are al- most exactly filled. The reason is that if the Fermi sur- face based on the free electron model approaches the zone boundary, then the development of the energy gap at that face lowers the energy of the occupied states relative to the unoccupied states and this stabilizes the structure. The criteria determining the efficacy of these two approaches to intermetallics would be considerably clarified if the Fermi surfaces of a number of them were known. As we have shown for AuSn, high-field galvanomagnetic effects can be used to study open orbits and to determine the state of com- pensation in intermetallic compounds. The experimental de- termination of the state of compensation, in itself, will be significant in the sense that any model of the Fermi surface must be consistent with this. Appendix A Bridgman Crystal Growing Furnace Fig. Al shows the Bridgman Furnace used to grow single crystals and the electronic control circuits used to stabilize the temperatures to i 1°C. -80- -81- 1; Ir I t 230 News / 12,-)/’r Recorder Con‘I’roIkr °\ T crmocoufks iii-Ii .:\ Lg; ~ N u.“ Dc‘I'QC‘I'or I I "E; CH: AMP Figure A1 Schematic diagram of Bridgman Furnace and electronic control circuits. Appendix B Crystallographic Angles for Hexagonal Crystals; 1.10 S c/a S 1.90 The following tables list the angles in degrees between the various crystallographic planes of hexagonal crystals for 1.10 S c/a S 1.90. Table BI. Crystallographic angles between planes (hlklll) and (h2k212) for arbitrary c/a. (210) (110) (120) (010) (100) 19.1066 30.0000 40.8934 60.0000 (001) 90.0000 90.0000 90.0000 90.0000 -82- PLEASE NOTE: Some tables pages are not original copy. Type tends to fade. Filmed as received. University Microfilms, Inc. Table BII . x. ' var“. ‘ . .- . o'bb AIO ' O‘ C ‘.O‘ A. 'O 1 C &O&.'_ ‘1. a. 0"\ g‘ .L»: 1'. AO.“Y ‘W. ‘ ' ‘ oOl‘a a‘YO e 1' Q a...) AIO s «'1 ‘ «LO‘l Iv. . . . $.55: ‘6. LOL/ 1". AOh-V A~JO LOO... A-‘O ' ‘.h.¢—. l—IO ' V ‘ l ‘ OO—Y A“. o I I a. ( o o I I I o Osaka Lu. .I—s.’ ‘U. 1 ’ a ‘Ow—IU AU. AOVO AV. T V *On—r'h Iv. ‘ O 4, AO‘U Al. ‘ 1 7 ‘.U-l LI. 1.-.] L‘. f, r- r» O O ( I I to r—- O O O O I \ *. O A y . O .I ( F O ' . ‘O‘YO AU. 10‘14. x... I ' ‘ ‘Ohlv A“. 5. -'~1 .54. ‘.‘.d 5“. Q I ‘ .0 tv .~_.O o " . .O'ln 4,--. O. f... Lb. V . o ‘.1-r 3“. 1 ‘ .‘ bOw‘d A.-. HHF—dh—‘h‘ O I -I J h. 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(continued) V v 1 ' 4...... $4.44 I -_-.—--._ ‘ i ‘O-cvl—u ‘4Ow-_.-v .._,_‘O. . - . ,. ‘Ovv ‘4014‘,’ 5-».-. ,, 1 , ‘ .. ‘O't ‘4O—JII—J ‘4-~.4O ‘4..— . lO‘I—d $4.444- HYOAUV *1 l O v ‘1 h— V . V I _ V I._ ' . _ . .4 . 'I O O ‘ d h— V O - .4! 4 V ~_ ’7 . ~_— V | - . ' u O O IN! w h— V O h l u ‘1 — O ‘ Q d O ‘- ‘ h V O ‘4 r ‘— H -— I O - — I L O ‘1 h- n— v O - .L --— \J — -. O V .. .4 1 I IL O 4 ~— I— - O .4 g. .4 y ~_ __ . . .4 3 O v ' ._ V O I I .4 _. .. -, . - _ I * O \— v 5— \,' O 4 I V a “‘ v O 4 v ‘I l ‘ O O ‘1 I — A O \4 4 V . u“ ._ . I .. __ O O u ‘4 _ L O _. v v— - ' O ‘ ' -- ' O O O ‘4 a ‘— -L O ~. 5. V ‘ — .4 O - d .— O O I V — a O 4 I 4 h x O L - , I I ‘ ' . C O l' O h— L O .4 ‘ v ‘7 —... .4 O - I .. A O I -— .— . o 4 ._ 4 l. -- 4 o ‘ J 4 , . l » A O I ‘4 6... 5 O I - . Q ~ ' ' I'\ ‘ z. i O I 1 L— ; O ‘4 - .4 v ._ I. . - v . I ~, . ‘ -~ O O I .4 §__ O V. 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I x; I 'I 5 .4 » I w --- I a - I U f I Crystallographic angles various planes for 1.10 1 . . - ‘ ‘ .— ‘ —. — . a h - U — r O ‘ - O ' ._- - . — , . .- , Q ' .. -. ». . w 0 _ _. ._ — —- v - . . ‘ - v - - J 5 . I U - 4 t— - .4 a -. 4 . - .s ' ». a 5 . v ' g ._ . . _ . tr — i ‘l ‘4 v . l - q - _. . , - , " ! ‘ ' V ‘ \r . ‘ -’ ‘ O J- ‘ -‘ . — - r- 1 — n . 1* ‘. ‘ ~ ‘ - V . -- - ‘ ‘ ; . . .— ‘ -.- ‘ . -- _r ‘ u ‘ ‘ f w l v ‘1 . ‘ ‘ G -— l ‘| . ~— I d ._. v J \- I ~ V . v a u v I O ‘ _ .. _ -.« V . t ~— v L . é -2 .a ~ 4 . . v ‘_ b V - v z ,. —- v ~ . o - -- - . o . ‘ - ._ _ ~ 'I ' , I I V ‘ . — — ‘1 y I . . v 51... _ - ‘ I 4 4 .1 w v . . ' .- g , I . , y. . _ - - I ' . I ‘4 I v ‘ . - I ~— I v . v , . , - ‘ . V d w- o ‘ v v -— 4 — . —_ 5 ~— _, .... ‘ . \.I 'T » _. . - v 4 7 I ‘— . .v 1., .... , \— ._ 1. us— . ' .1 - 0 ~ . '7 \- ; ‘ v s _. , _. .__ . . _, V - . _ . .4 ' v ‘4 -—. — — v __ . A .... ~— - . —. _. -. .4 ~— d — ~4 . u v 5 - . u - u— _ Ar . a g , ~ ~_ . ' . a l - O b w l v - - _ .1 ~— v Q ' ’ d. I .. O J l y J ~ - h. ‘1 .. _. . .. .. V J . ~ . \I I s v --' ‘- " . v ‘ v v . I a .. ~- A v . ‘ I 5 I .- .. ‘ l .._... ‘ *1 ~— . - w 5..., -.._ 1 - . _ 1 v.. "I' M .— v v v - . ‘ .- ,, . - . ‘1 f V v ‘4 ' u r V ~— . 5.. _‘ ._ .4 . ~.. . v p - ‘ n a ,1 ’u— . -' 1 h— I U . v w‘h ‘ —' . . . - w ‘4 ’ . - _ . 'v I v . ‘- -_, _/ " .4 ' I l f ‘ v . ‘ . c _ v a , v . . ‘v ' \J v ., - o “ ' -’ Y . ~» - — 0 '- r g x. . . . . . m . . .-< o _, . . ._ q , _. v _ .. - . ‘ I (~ *~ v~o‘ »e- --o-.-7 -.- _ . A ', , x v . v “‘1‘ v .... . V . t I . . ,, .v . . _. _ -—. 1 . ‘ - . I .. '- ._ .4 ~ ~ . ' v‘ 4. _. : I O Q.— I -r 5 v ~ v .. u w o - ? .4 , I . o ‘1 - _. x w .. “p ' ‘- 0 ‘ - ‘ v . I o r ' a. ‘ V _. . b ‘ V' . ‘ —‘\-l v I ; . w h _ \- ‘_ ‘ r‘> ; . r ‘- v ‘1 L . ‘— — ‘ \_. I ' . V V ’ _ \J v —. . I 1 O . ‘, ' r‘ ,A \J V . -... L J I , . V ‘ v v ‘. . between (001) and S c/a S 1.90 p. '.. .4 Table BIII. (continued HHF—‘O—‘O—‘P‘ F; *0 F. r4 b—- o-—- o- *.L on 0“ o»- r ...l 4 r« 04 v. r4 o» ’ a or m U u cm L:- ( ( (Lt ( p..- h. Okf \JC'L‘I H IMHO u L. p- '-1 \10 (.1 N ( \ *4. y»: .‘_-. @114. "L- #4. \’.~ ,~ UkJV“? (\ ( F ( ~J F. 1 ~— ‘ u '4 H ‘ ‘ U ’ r ~ I l v ’$——l -v II-» -' -l_ ., A --V v I 4——————.« - \4 ' — v _, - ’ b h- _ P V».4‘a_ g4“? 131 -Q; ._. -,_, ‘V. &—'u 9 .a‘ w... -‘.v.4 y- — ‘— . A ... -- ‘- 7 ' . — _: .. ‘— v 4 .--O (i\ A Appendix C Extraction of Hall and Transverse Even Voltages from Transverse'Voltages Let Vt(I,B) be one of the transverse voltages as measured, for example, across probes l, 5 in Fig.9 3 I is the sample current and B the magnetic field. Now Vt(I,B) = v (c1) H + Ve + V T where: VH Hall voltages = transverse voltage changing sign with I and/or B. Ve = even voltage changing sign with I but not B. VT = thermal emf in potential leads. Ve consists of two parts: V = 'V e TE (02) + vmis ’ where VTE is the transverse-even voltage which is pro- portional to B2 and Vmis is the (Ir) drop due to mis- alignment of the transverse potential probes. Upon re- versing the direction of the sample current and magnetic field, we have V£(I,B) — VH +‘Ve + VTl Vt(-I,B) = --vH - ve + le (c3) Vt(I,-B) = --vH + ve + vT2 Vt("'I,-B): V - V + V _88- In writing these equations we have assumed that Vt(I,iB) and Vt(-I,iB) are measured essentially at the same time so that the thermal voltage has not changed upon changing the direction of the current. However, since the direction of the field is changed with some difficulty in a super- conducting solenoid, VKiI,B) and V(iI,-B) may be measured at times differing by several hours; therefore, a dif- ferent value of the thermal voltage is used for the two different directions of field. If we define Avi '5 Vt(I,:i:B) - Vt(-I,:!:B) (05) then uvH = AV+ - AV_ (06) We = AV+ + AV_ (c7) VTE can be extracted from Vé by determining Ve = Vmis when B = O. The above equations show that the effect of thermal emfs goes out if we measure the quantities AVi. Since the thermal emfs are as much as 0.5uV and the Hall voltages are only of the order of microvolts, it is very necessary to measure the transverse voltages as described above. Appendix D The Hall Effect at a Singular Field Direction Consider a compensated cubic metal having the Fermi surface shown in Fig. D1. The hole sheet of volume V“ is h multiply-connected and the electron sheet of volume v; =‘Vfl is closed. Let the field be along the z axis. There are no Open orbits for this direction of field. As in (28) the Hall effect measures the quantity v = Ve _ Vh = [[Aeficz) - Ah(kz)]dkz . Now for ~d/2 s k S d/2, there are only closed electron orbits Z on the hole sheet of the Fermi surface. Therefore, for this direction of field .. ' _ f '- Vh "' Vh ] A\1nocc(1‘z)dh{z and v6 = Vé + [Aocc(1{z)dkz , where Aunocc(kz) and Aocc(kz) are the unoccupied and occupied areas of the hole zone reSpectively, intercepted by the plane kz = constant. Thus ‘V = 'Ve - Vh = Vé ' Vh +erAocc(kz) + Aunocc(kz)]dkz ' But Vé - VA = O, and Aocc(kz) + Aunocc(kz) = ABZ(kz) = A = b2‘ -89- -90- Hence V = ijBZ(kz)dkz 2 and for the simple Fermi surface of Fig. Dl, V = Ad = b d. It is therefore seen that at a singular field direction, the sign of the Hall coefficient is determined by the char- acter of the closed sheet or sheets of the Fermi surface. -91- 2 v “‘————“ electron “‘-—————”’ volume‘Vg V ’ A z I 9 holes volume V' J/ h 1 ___..__/ ‘A‘II’V h_' k2 = 0 d d b b Figure Dl Simple compensated Fermi surface. ll. 12. 13. 1A. References A. B. Pippard, Trans. Roy. Soc. (London) Aggg, 325 (1957). I. M. Lifshitz, M. Ya Azbel', and M. I. Kaganov, Zh. Eksperim. i Teor. 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