MOLECULAR FORCES AND ELASTIC CONSTANTS OF POLYETHYLENE SINGLE CRYSTALS Thesis for the Degree of Ph. D. MICHIGAN STATE UNIVERSITY .Ioginder N. Anand 19.6.6 'mrcrs ABSTRACT MOLECULAR FORCES AND ELASTIC CONSTANTS OF POLYETHYLENE SINGLE CRYSTALS by J oginder N. Anand Lamellar polyethylene single crystals have a folded-chain structure in which planar zigzag segments of molecules take an orthorhombic lattice. For these crystals, nine independent elastic constants appear in the generalized Hooke's law. Thus, they are inherently quite anisotropic. Their anisotropy is enhanced further by the directional intra- and intermolecular forces. Intramolecular forces are due to the covalent C-C bonds forming the chains, and are much stronger than the intermolecular London dispersion-type of van der Waals forces. The latter have been approximated by a 6-12 Lennard-J ones potential involving two unknown constants; the ratio of which is fixed by the equilibrium separation to give a minimum in the potential. Their values are determined by comparing the computed crystal potential energyand the experimentally-determined cohesive energy, and are found to be comparable with those of argon. First and second nearest-neighbor interactions are considered to derive finite difference expression for the components of the force acting on a unit in terms of relative displacements and interaction constants. These are converted into partial differential equations and compared with the corresponding equations of motion obtained from continuum theory to establish relationships between the elastic J OGINDER N. ANAND constants and the interaction constants. A limited central force assumption is employed to reduce the number of interaction constants from thirty to fourteen for the second nearest-neighbors and from eleven to seven for the first neighbors only. Interaction constants for units belonging to the same chain are obtained in terms of the C-C bond stretching, bending and repulsive force constants while others are obtained from the 6-12 potential in terms of the Lennard-J ones constants and the appropriate separation distances. Finally, by substituting values of the intra- and intermolecular force constants and the geometric parameters, numerical values of the interaction constants and the elastic constants have been obtained. From these the values of Young's moduli E1, E2 and E3 obtained in directions a, b and c, are found to be about 0. 38 x 10-6, 0. 27 x 10"6 and 2. 39 x 10-4 dyne/AZ respectively; while the constants C44, c55 and C66, identified as shear moduli, have been calculated to be 1.12 x10-4, O. 89 x 10-4 and 6. 52 x 10-7 dyne/Az. The magnitudes of the constants c23, C13 and CM. are found to be equal to those of C44, c55 and C66. The value of E3 for the chain direction compares well with the Young's modulus of oriented polyethylene obtained theoretiCally as well as experimentally. Furthermore, the value of the Young's modulus of bulk polyethylene lies between the values obtained for moduli along and across the chain. It is interesting to note that polyethylene single crystals are found to have shear resistance even when only first neighbor interactions are considered and forces are central. MOLECULAR FORCES AND ELASTIC CONSTANTS OF POLYETHYLENE SINGLE CRYSTALS by J oginder N. Anand A THESIS Submitted to Michigan State University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Metallurgy, Mechanics and Materials Science 1966 ACKNOWLEDGEMENTS The author is very grateful to Dr. T. Triffet for his continued guidance and assistance throughout the course of the work which made this thesis possible. He wishes to thank him for acting as thesis advis or and chairman of the guidance committee. He also wishes to extend thanks to the members of the guidance committee for their helpful suggestions and interest in this work. ii TABLE OF CONTENTS Page ACKNOWLEDGEMENTS ....................... ii LIST OF FIGURES .......................... iv LIST OF APPENDICES ........................ v I. INTRODUCTION .......................... 1 l. l. Crystallinity in Polymers ................ 1 1. 2. Polymer Single Crystals and Related Structures . Z l. 3. Polyethylene and Its Single Crystal Structure ...... 4 1. 4. Anisotropy of Polyethylene Single Crystals ....... 10 l. 5. Objectives ......................... 10 II.‘ THEORETICAL DEVELOPMENTS ........... . . . . . l3 2. 1. Elastic Constants of Polyethylene Single Crystals . . . 13 2. Z. Intramolecular and Intermolecular Force Constants . . 21 2. 3. Interaction Constants and Elastic Constants . . . .‘ . . . 31 Z. 4. Interaction Constants and Molecular Force Constants. . 50 2. 5. Numerical Values of Constants ............. 59 III. DISCUSSIONS OF RESULTS ................... 65 3. 1. Anisotropy of Polyethylene Single Crystals ....... 65 3. Z. Continuum Theory of the Orthorhombic Lattice ..... 65 3. 3. Molecular Forces .................... 67 3. 4. Interaction Constants ................... 70 3. 5. Elastic Constants ..................... 73 IV. CONCLUSIONS .......................... 76 V. FUTURE EXTENSION OF RESEARCH .............. 80 VI. BIBLIOGRAPHY ......................... 103 iii an "IV .11 Figure l. l 1.2. 2. 5. 2. 6. 2. 7. 2.8. 2.9. 2. 10. 2. ll. II-1 IV-1 LIST OF FIGURES Page Fringed micelle model ................... 3 Configuration of linear polyethylene ............ 4 Tetrahedron formed by the four bonds of carbon ..... 5 (a) Planar zigzag conformation (b) chain folding ..... 5-6 Schematic diagrams (a) flat (b) hollow pyramid, lozenge- shaped, platelike polyethylene single crystals having a folded-chain structure (c) hedrites ............ 6-7 Schematic representation of the unit cell of polyethylene . 8 Entangled-rectangular cell structure (a) and (b) ..... 9-10 Reduction to simple orthorhombic lattice ......... 13 Equivalent lattice with (-C2H4—) units occupying lattice pctnts ............................ 14 Lennard-Jones 6-12 potential curve (Mr) and force curve F(r) ......................... 24 Schematic representation of two—dimensional lattice structure ...................... 27 First nearest-neighbors in first quadrant only ...... 33 Second nearest-neighbors in first quadrant only ..... 33 Rotation of x'y'z with respect to x y z ........... 34 Rotation of x"y"z with respect to x y z .......... 34 Geometrical representation of axes xij ......... . 41 Geometry of two corresponding C-C bonds ........ 51 Deformation of C-C bonds ................. 52-53 Rotation of axes . . . . . . . ............ . 90 Detailed drawing of chains in lattice in plane (a, b) . . . . 101 iv LIST OF APPENDICES Appendix Page I. EvaluationofSeries................ 82 II. Transformation of Partial Derivatives . . . . . . 90 III. Strain Energy Connection Between Elastic and Interaction Constants . . . . . . . . . . . . . 96 IV. A Note on the Lennard-Jones Potential . . . . . . 100 a... nu. "II A a...‘ 4 1.. ‘ 1., “1‘ ‘ I fly, a.‘ I. INTRODUCTION 1. l. Crystallinity in Polymers It has been found that most polymers, perhaps all, are partially crystalline, having co-existing ordered and disordered regions (1). Their x-ray diffraction patterns show both sharp features associated with regions of three-dimensional order, and more diffuse features characteristic of molecularly disordered substances like liquids. The degree of crystallinity can be estimated from changes in density, specific heat, refractive index, transparency, x—ray diffraction patterns and various other physical properties. In fact, many of the unique physical properties of polymers are associated with their ability to crystallize. Stereoregular isotactic polymers whose molecules are chemically and geometrically regular in structure, such as linear polyethylene, are typically crystalline. Noncrystalline polymers, on the other hand, include those in which irregularity of structure occurs, such as atactic polymers or copolymers with significant amount of two or more quite different monomer constituents. Unit cell data and other information, such as the configuration or chemical structure and the conformation of several crystalline polymers, have been compiled by Miller and Nielson (2). In a number of new isotactic polymers two or more conformations and unit cells have been observed to depend upon the temperature and other conditions of crystallization. The most commonly occurring unit cell structures in various polymers may be classified as orthorhombic, pseudo- orthorhombic, triclinic, hexagonal, monoclinic and rhombohedral. l. 2. Polymer Single Crystals and Related Structures Crystalline polymers usually crystallize from dilute solutions in the form of thin lamellae called single crystals; and such crystals of many polymers such as gutta -percha, polyethylene, polypropylene, polyamides,cellulose and its derivatives have been reported since their independent discovery and identification in 1957 by Till (3), Keller (4), and Fischer (5). All polymer crystals have the same general appear- ance, being composed of thin, flat or hollow pyramidal platelets. Spiral growths of additional lamellae originating from screw dislocations are usually present on their surface. Crystallization conditions such as solvent, solvent concentration, temperatur'eand rate of cooling determine the size, shape and regularity of these crystals. However, their‘thick- ness depends mainly on the crystallization temperature and any subsequent annealing treatment (6)- . Electron diffraction analyses of these crystals indicate that the polymer chains are normal or nearly normal to the plane of the lamellae (3, 4, 5). The length of polymer chains being several times the thickness of a lamella, Keller (4) points out that the molecules must be folded back and forth on themselves several times. In polyethylene, for instance, the molecules can fold in such a way that only five carbon atoms are involved in the fold itself (6 ), as shown in Figure 1. 4 (b). When the rate of growth during crystallization is slow, relatively thick aggregates of single crystal lamellae having a common nucleus and orientation, called hedrites (Figure l. 5 c), have been reported for polyethylene and polyoxymethylene (7, 8, 6 ). They have a polygonal appearance, and are the closest approach to a macrosc0pic single crystal. But at faster growth rates numerous defects, such as vacancies and interstitials, terminal groups, branches and improper folds, are incorporated into the lattice. During crystallization from the melt spherulites develop which have a complex lamellar structure, as seen in the electron micro- scope (9). Their nuclei have a random orientation, and growth occurs radially outward from these until the entire volume is filled. When two spherulites meet during crystallization they form a common straight boundary in which the transition in orientation takes places (1). This picture, known as the "crystal defect solid" model of crystalline polymers, visualizes the matrix as an ordered region having defects incorporated throughout (1). It is in direct contrast to the old "fringed micelle" concept, in which a crystalline phase consisting of crystallites is taken to be embeded in an amorphous matrix forming a second phase. In the 1atter.molecular chains are visualized to pass through several crystallites and, thus, to have several straight and several disordered segments, as shown in Figure 1.1. .11 ‘ a /% Figure 1.1. Fringed micelle model. ) I; .— r5... ‘.‘-~I‘ ;’e .ao-ltvta - . -~ u. ‘v. .” --.. s-s ‘ 9 :h‘oeqp .. Ms ~ A ll -1 f? I EX‘v I ‘d‘. . I "" VA NI ‘CV Although from a macroscopic point of view it may appear that at low crystallinities both concepts are identical, as far as a microscopic description is concerned the two are completely different. 1. 3. Polyethylene and Its Single Crystal Structure The chemical formula of polyethylene is CnH2n+2' Thus, a poly- ethylene molecular chain consists of n, - CHZ- chemical repeat units, neglecting the end ones. The configuration of a linear molecule is shown below in Figure l. 2. H H H H H H I I I I I I H-C -C -C -C-C-C— l I I I I I H H H H H H Figure l. 2. Configuration of linear polyetheylene. This may also be abbreviated and written as (-CH2-)n . Covalent single bonds formed by the sharing of two electrons, exist between two consecutive carbon atoms and between carbon and hydrogen atoms. The length of the C-C bond is about 1. 54A, slightly longer than the C-H bond length of about 1. 10A. Carbon is tetravalent and its four bonds are directed in space in such a manner that it lies at the center of a tetrahedron as shown in Figure 1. 3. .H 1.54A C Tetrahedron formed by the four bonds Figure l. 3. of carbon. The angle between any two bonds is approximately the tetrahedral angle of 109°28', as shown. Carbon atoms forming the backbone of a linear polyethylene molecule take up a planar zigzag conformation mm crystal lattice, as shown in Figure l. 4 (a). 109°28' T] repeat distance Figure l. 4(a). Planar zigzag conformation. Figure 1. 4(b). Chain folding involving five C atoms. The repeat unit is (~--CHz-CH2 -) or («C2 H4-) and the distance between two alternate C atoms is the repeat distance; it is approximately equal to 2. 55A. Polyethylene single crystals crystallizing from dilute solutions have well defined forms, which usually consist of lozenge-shaped flat or hollow pyramids lOO-ZOOA in thickness and about 10-20 microns in lateraltdimensions: lOO-ZOOA lO-ZOp Figure l. 5(a). Schematic diagram of flat single crystal. I I (b) lO-ZOp (C) 100p. J r“ '7 Figure l. 5. Schematic diagrams (b) hollow pyramid, lozenge-shaped, platelike polyethylene single crystals having a folded-chain structure (c) hedrites. The molecular chains forming these crystals have a fold-length of the order of the thickness of the crystals (4). The unit cell structure of polyethylene is orthorhombic, and i. 3 Shown in Figure l. 6 (a, b, c). ,’ (a) c -axi ~axi s a -axis (b) (C) Figure l. 6. Schematic representation of the unit cell of polyethylene showing (a) parameters a, b and c (b) location of molecular chains along the c-axis and (c) setting angle of 41° that the planes of chains make with the b-axis. ... II) I n —,.o - has \ D'. ' '- 6. I ‘I:v1 .8...‘ 6»: us .C Axes a, b, and c are orthogonal and the respective parameters a, b and c are approximately 7. 41 A, 4. 94A and 2. 55A at room temperature, as determined by x-ray diffraction by Cole and Holmes (10). Molecular chains lie along the c-axis, thus, c is just the repeat distance. The unit cell consists of four parallel planar zigzag chains running along the c-axis at the four corners of the (a, b) rectangle, their planes making an angle of (3 = 41 o, with the b-axis, as determined by Bunn (11), and one running through the mid-point of the rectangle having a different orientation from the other four. The chain through the midpoint of the rectangle and three additional similarly-oriented chains through the midpoints of adjacent rectangles may be considered to form their own (a, b) rectangle. Thus, the entire crystal may be considered to consist of chains having these two orientations, their respective rectangles forming an entangled cell structure as shown in Figure l. 7 (a and b): 41 Figure l. 7(a). Entangled-rectangular cell structure. A f " Ink/a . fi‘:t ..“‘ ...'., s~.:‘ - :I‘I‘V‘ \ .‘) ”an. ‘nz‘. Fa‘ “a "I‘h. \IH . “I U»... in. k‘. 10 Figure l. 7(b). Entangled-rectangular cell structure. 1. 4. Anisotropy of Polyethylene Single Crystals For the class of crystals having an orthorhombic lattice, the 36 constants of the generalized Hooke's law are reduced to 9 independent constants, as against 3 for crystals having cubic symmetry (12). Anisotropy of such crystals is, thus, much more complex. Besides, polyethylene single crystals have another feature, peculiar to poly- meric crystals, which contributes to additional anisotropy. In the direction of the c-axis, or along the molecular chains, the primary covalent C-C bonds, are several times stronger than the secondary bonds existing between any two molecular chains due to the weak van der Waals forces (13, 6). This difference is superimposed on the inherent anisotropy of the orthorhombic lattice structure. 1. 5. Objectives A connection between the nine independent elastic constants, sl ,, n.» .. o'I-g" a‘. I 1 I s cm” 1,6. sealvlol 5;:g.e cr ‘ a._.~y-D Lyvsu . e .~. 6. '6 .vuu hGAsb . . '3‘ 9,. 1 4‘. Nae - .; :2 rs: b< vas- ., \ .3 den". n. ’11 ’I , 11 as they appear in the generalized Hooke's law, and the microscopic intermolecular and intramolecular force constants is obtained for single crystals of polyethylene in the present work. However, in accomplishing this objective the continuum or macroscopic elastic constants are obtained first in terms of interaction force constants, for the forces existing between units occupying the present orthor- hombic lattice, by following the von Kafrma'n cubic crystal structure : J L“! approach (14). First nearest-neighbor and second nearest-neighbor inter- actions are accounted for, and the effect of central force assumption ' J is demonstrated. The interaction force constants are in turn obtained in terms of the more basic constants, such as stretching, bending, torsion and repulsive force constants for the primary C-C bonds that exist along the molecular chain axis, and the intermolecular force constants for the net attractive forces between adjacent chains due to secondary bond forces. The strength of the C-C bonds under various types of deformation is well-established, by Mizushima and Simanouti (15). However, the strength of the secondary bonds is not known for polyethylene. The net potential existing between adjacent chains is approximated by a‘: 6-12 Lennard Jones potential (6), which involves two constants whose ratio is determined by the equilibrium distance of ” the two chains. Their exact values are then determined by calculating the crystal potential energy density and comparing it with the experimentally-determined value of the cohesive energy density for polyethylene (16 ) . 12 Numerical values of the interaction constants are obtained from the values of the C-C bond strength constants, the Lennard- Jones potential constants and the geometric parameters. These are then substituted in the expressions for the elastic constants to yield their numerical values. The nine independent elastic constants of the generalized Hooke's law are measures of the Young's and shear moduli of polyethylene single crystals in various directions. These are compared with known values of the constants, such as the Young's moduli of oriented and bulk polyethylene. Shimanouchi, et al. (17) have calculated the Young's modulus for oriented polyethylene, consisting of infinitely long molecular chains, to be 3. 4 x 10P4 dyne/Az. This is somewhat higher than the value of 2. 6 x 10-4 dyne/A2 determined experimentally by Dulmage and Contois (18), using x-ray diffraction and the relaxation technique. The values of the Young's moduli along other directions should be considerably lower than this, because the forces existing along other directions are much weaker. The Young's modulus of bulk crystalline polyethylene is of the order of 10.5 dyne/Az, and this must represent some kind of an average of the moduli of polyethylene single crystals along the three lattice axes. Like the Young's moduli, the shear moduli too should be higher along the chain direction. II. THEORETICAL DEVELOPMENTS 2. 1. Elastic Constants of Polyethylene Single Crystals In the orthorhombic lattice structure of polyethylene, as discussed in Section 1. 3 and illustrated in Figures 1. 6 a-c, four molecular chains having parallel orientations and one having a different orientation occupy, respectively, the four corners and the center of the rectangle (a, b). This may be reduced to a simple orthorhombic lattice by considering pairs of two chains, consisting of one at the corner and the other at the center of the rectangle, to occupy~ lattice points, as shown in Figure 2.1. This reduction. Figure 2.1. Reduction to simple orthorhombic lattice. Lattice points are occupied by units of two chains connected by a natural fold. facilitates the application of symmetry operations to a polyethylene .- single crystal. . since then the crystal would have the same number of symmetry elements as a simple orthorhombic lattice cell structure. It may also be noted that a chain lying along the c-axis can be broken into (-C2H4-) repeat units without any loss of generality and, as shown in Figure 2. 2, the equivalent lattice structure is then an orthorhombic structure with units occupying the lattice points. 13 n.‘ \ 'H 'V l4 ”lag. Figure 2. 2. Equivalent lattice with (-C2H4-) units occupying lattice points. We are now in a position to write Hooke's law with proper symmetry operations for polyethylene single crystals. For small strains ,Hooke's law states that stress is proportional to strain and for an anisotropic medium its generalized form may be written mathematically as 0'. = c. 6. 2.1 The constants of proportionality cij are called the elastic constants or moduli of elasticity, while (Ti and ej respectively represent the stress and strain components. Equation 2. 1 may also be solved for strains in terms of stresses to obtain 15 and elements sij of the inverse matrix are called the moduli of compliance. The 36 elastic constants in Equation 2.1 are reduced to only 9 independent constants (12, 19) for the symmetry elements of an orthorhombic lattice. These nine constants are shown in the matrix given below y—I — C11 C12 c13 0 0 0 c21 czz c23 o o o c c c 0 O O Cij ___ 31 32 33 2.3 O 0 0 C44 0 0 o o o 0 CSS 0 0 0 0 0 0 C66 wh : : : ere c:12 CZl’ c13 C31 and C.23 c32' Equation 2.1 may now be written out by using this matrix: “1 = “11'514r C12 €2 + C13 63 cr2 = C12 61* C22 E2 + C23 63 “3 = C13 61 + C23 '52 + C33 63 2.4 “4 = C44 64 “5 = c55 ‘5 ‘6 = C66 66 L . ettlng u, v and w be the components of displacement along the ax es 3:. y and 2, respectively, where these correspond sequentially with the parametric axes a, b and c, we may write the strains Ei .- (i. I - ‘3624 lher ZI‘ Q C.‘ {v \. l6 as -3_u - 2! -E’fl 6l - 3x ' 62— 8y ’ 63 -32 and 2.5 8w 3v Bu 6w _8v Q3 64-3??? 93-575? 66-3.. *3, Also, it may be noted that a 64 z Y23 E 65 : l’13 66 : le 2.6 Where the Yi-'8 are shear strains. Young's modulus E and the Shear modulus G are defined by Where 0' and E are the longitudinal stress and strain, and 2.8 Where 7 and Y are the shear stress and strain. Applying this to the particular case in hand, we obtain three Young's moduli El' E2, E3, and three shear. moduli G23. G13. and G12 as shown below. Rewriting the first of the six expressions in 2. 4 as for 1111' - lab-(13,1 stress 0'1 only E161: or1 : C1161+¢12€z ”1363 2.9 and - dlviding both sides by cl. we get ’ESS D 1!: s 17 € € _ 7- __3_ I51 ’ C11+C12 61+C13 e1 Similarly, by repeating the above operations for the other five expressions in 2. 4, we get 6 6 E2 = C125+‘322J'023E; 2.10 6 6 _ _l_ .3. E3 “ C13s +C235 “:33 3 3 and E4 : C44 z 23 5 = C55 = (:13 2.11 E6 = C66 = G12 6. v..=-—-1-=--—1—=-1—— 2.12 13 e. e. V. J _.1 11 6. 1 to get six vi.'s, such that V - :1 V _ _ 5.2. 12 62 21 61 6 E 3 1 U : - — , V : - -— 2.13 31 61 13 63 6 6 ”23 = ‘ _Z ' ”32 = ' El 63 2 $11 IbST—‘ituting 2.13 in 2.10, we obtain: E1 : C11 ”‘12 ”21 ' C13 ”31 E2 = C22 ‘C12”12 ' C23 ”32 2'14 ”F1‘L'i:~.ikl-mmmnu ‘ . - . . 3 ’0 K.__, , a . , 1“" MI on 3 J ‘3 . U) a. RI. cs. ec The Vij's may be evaluated in terms of the cij's by using simple uniaxial stre 3 se 3 . 0’ Solving the last two equations of 2.15 and similarly by considering uniaxial 21 31 C c €+c €+c E C dlre<:1:ions, we obtain: 32 12 13 23 ll 12 136 m HN m m u.) p—a m m NU) m "‘l N H m "‘l oar—- m m CON €+c €+c E l l 1 18 Thus, considering a uniaxial stress 1 along the x-direction, 2.4becomes 122133 222 233 + C23 62 + C33 63 C C33 C12 C23 13 ‘ , 2 C33 C22 " C23 (:22 C13 " C12 C23 " 2 C33 C22 (:23 C11C23 ' C13 c12 _ c 2 C11 33 '°13 C33 €12 ' c23 C13 ' 2 C33 C11"°13 C22 °13 c12 c23 22 C11“ c12 c11 C23 C12 c13 11 22' 12 2.15 simultaneously, it follows that: stresses in the x and y- 2.16a a- O u “4 1“- TV},G l9 ' Substituting 2. l6.in 2. 14 gives: °12(°23°13 ' °33°12) + °l3(°12°23 ' °22°13) 1:31 = °11+ 1 7‘) °22°33 ' °23 2 2 _ 2 C12 °13 °23 ' °12 °33 °13 °22 = c + 11 (C C _ c 2) 22 33 23 + 2 2 2 _ C 2 °11°22°33 °12°23°31 ' °12°33 " °23°11 31°22 2 (°22 °33 " °23) 2.17 Similarly, E2 and E3 may be obtained by considering uniaxial stresses 0'2 and 63intle y and z-directions; they are: + 2 Z c 2 - c 2c E °11°22°33 °11°23°31 ' °12°33 ‘ 23°11 31 22 2 _ 2 ' (C11 °33 " °13) 2.18 ccc +2ccc --C2 c2 -c2 E 11 22 33 11 23 31 12°33 23°11 31°22 3 - . 2 (C11 C22 ' °12) 2.19 It Should be noted that (c c -c2)E=(c c -cz)E=(c c -c2)E 22 33 23 l 11 33 13 2 ll 22 12 3 2 2 °11°22°33 + °11°23°31 ' <:12°33 2 2 ' °23°11 ' C31°22 2'20 Later in this work expressions for the elastic strain energy and . . . . . . equatlons of motion W11]. be needed for comparison w1th equations Obt - 3‘ lhed from microsc0pic considerations, in order to evaluate the interaction force constants . 20 strain energy density U, we note that all of which may be Thus, and on C on U as Q) m y—I II q N 1 2 2 2 U ‘ 2(°11°l +°22°2+°33°3) ’+(°12°1°2'+°13°1°3'+°23°2°3) +1—(c e + e + 62) 2 44 4 °55 5 C66 6 aU _ _ 361 " C11°l+°12°2+°13°3 “l 3U _ _ 862 " C12°1+°22°2+°23°3 " “2 aU _ _ 353 ’ °13°1'*°23°2'*°33°3 ‘ “3 8U _C E _6 EU _C _a aU 3124‘ 44 4' 4' 355“ 55 5‘ 5' 356 obviously satisfy 2. 21. To get such an expression for the elastic 2.21 satisfied if U takes the following form: 2.22 2.23 °oo°o ' “6 ' Now, the equations of motion may be written in the form '(‘12,‘ 14): fi: aal+3€£+€i§ po 3i av az 3215 not L $53. 21 . _ 8176 + 80'Z + 864 p0 8x 8y 82 80' 80' 8a .. _ 5 4 3 p w - Tx + “8y + —8z 2.24 where po is the density. To Specialize these. equations for an orthorhombic lattice, we must substitute 2. 4 and 2. 5 in these, the result is: azu a2u an2 av2 8W2 "o"i = °11 3x2 + °66a y? + °55 :2 + (°12+°66)ax_Y" av +(°13"°55)'z§“'_xaz 62v 82v av2 3“2 3va po I ' °66ax 2+ °22 "'2' + °44 :2 + (°12+°66) 8x8y + (°23+°44)"'"" 8y82 2 2 2 2 2 __ 8 w 8 w 8 w 8 u 8 v Pow ’ °55 a")? + C44—Tay + C33——8z2 + (°13+°55) 8x 82 I (°23 °44) av" 62' 2.25 Since the orthorhombic lattice has nine independent elastic constants cij instead of three, like a simple cubic structure, expressions for the Young's moduli, shear moduli, POisson's ratios, Strain enerSY. and equations of motion are naturally much more in"(fl-Ved. 2' 2 Intramolecular and Intermolecular Force Constants Various molecular force constants are described in this section, and a. procedure is developed for calculating some of them which are not known. In Section 2. 4 the. macroscopic elastic constants c J dis c"flesed in Section 2.1 will be obtained in terms of the above- me - htl oned microscopic force constants; for this purpose the two 22 following types of forces are important: (1) Intramolecular or primary bond forces (ii) Intermolecular or secondary bond forces i) Intramolecular Forces The carbon atoms constituting the backbone of a linear poly- ethylene molecule are held together by covalent bonds formed by sharing pairs of valence electrons. These C-C bonds feature the primary or intramolecular forces with which we will be concerned. The other covalent bonds are carbon-hydrogen or C-H bonds by means of which hydrogen atoms are held to carbon atoms. The C-C bonds have a length of 1. 54A, as against 1.10A for the C-H bonds, and they serve different purposes insofar as their contribution to the strength of the crystals is concerned. The strength of a polyethylene chain depends entirely on the strength and degrees of freedom of the C-C bond. On the other hand, because "of its geometric and steric configuration, the C-H bond plays an important role in determining the c rystal structure and providing the intermolecular electrokinetic fox-c e s to be discussed later. In a polyethylene molecule all four valencies of carbon are 8-at7i»131:'ied and its four bonds are directed in space as shown in F o 181“are 1. 3. In general, segments of this molecule are free to rotate a bout the C-C bond in such a manner that any three carbon atoms always to nth a plane. However, as described in Section 1.3, the molecular Cha ~ 11:18 take up a planar zigzag conformation in polyethylene single "Ya . tals and thereby prevent any rotation about the C -C bond. n 9 me ’I\ .ve “6 o- :t‘ I the 0V Tie I 23 The strength of C-C bonds for various types of deformation has been determined by Mizushima and Shimanouchi (15), and values for these and other geometric parameters are listed in Section 2. 5. The force between two alternate chemical units of -CHZ- along the chain axis is repulsive due to their being too near each other. In the absence of any free rotation about the C-C bond, deformation of molecular chains will take place by a process of deformation involving stretching, bending and repulsive force constants only. This fact will be made use of later in Section 2. 4, to obtain the interaction force c onstants. ii) Intermolecular Forces As discussed in Section 1. 3, the crystal lattice of polyethylene is such that adjacent molecular chains occupy an orthorhombic cell. The attractive forces between these chains, which bind them together in the solid crystalline form, are called the intermolecular or Sec ondary valence forces. Polyethylene is a nonpolar material for two reasons. First, because all the valencies are satisfied and, second, because both Garb on and hydrogen are equally electronegative. Therefore, the attractive intermolecular force is not due to permanent dipole moments, but rather to time varying dipole moments resulting from diffe rent instantaneous configurations of the electrons and nuclei. The a . . , . . e are also called London dispersion forces, the potential govermng them is proportional to the inverse sixth power of the distance (20). Between any two molecules, there is also a repulsive force due to the interference of the electron clouds surrounding the nuclei. 24 This force is short-range compared to the London attractive force, decreasing exponentially with distance (21, 22, 23). At the equilibrium separation the net force is zero; and, of course, the net energy, or the potential curve, will have a minimum at this distance. Different portions of the exponentially-decreasing repulsive potential function may, for convenience, be matched by different inverse powers of the distance (24, 25). If for polyethylene, as suggested by Geil (6), we approximate this potential by the twelfth power, the total potential energy function 4) may be written as d>(r) = 315—- %, 2.26 r 1‘ where r represaits the separation distance and A and B are constants called the Lennard-Jones potential constants. This is the standard form of the Lennard-Jones 6-12 potential (26). Evaluation of A and B the Lennard-J ones Constants The shape of the general potential curve ¢(r) is as shown below: (r) IF(r) Figure 2.3. Lennard-Jones 6-12 potential curve (Mr) and force curve F(r). gives DI 25 The gradient of ¢(r) will give the force F(r) between two adjacent molecules. Thus, we may write - 92.111 2.27 F(r) : dr or F(r) = ”if; - 9-?- . 2.28 r r The curve of F(r) is also shown in Figure 2. 3. The force F(r) being zero at the known equilibrium distance r0 imposes the condition that the constants A and B have a certain definite ratio; F(r) = 0 2.29 give 8 3 - T: O 2.30 O 01‘ E- r . 2.31a wiere I npg ass in; 3 u ._ , .gtqv , A r 'VVvs a ' ‘ Y P'D‘ — ~...C.. 11"3'53 Lethe 2:85 .1. ...e C i me e: :ccu: 3.151 26 Rewriting 2. 31a a's A=pB, 2.311) 6 where p = i— ro is a known constant, 2. 32 and substituting for A in terms of B from 2.31b in 2.26, we obtain the potential ¢('r) in the form ¢ = 3% - 135. 2.33 r 1' which involves only one unknown constant. The constant B can now be determined by computing the crystal potential energy density, in a manner similar to that used by Lennard-Jones (26) for cubic crystals, and by comparing it with the cohesive energy density—an experimentally-determined value (16). The crystal potential energy density, denoted by E, is defined as the energy per mole of polyethylene,in which the individual units occupying the lattice points are surrounded by an infinite matrix. It is computed by summing the lattice energy of the individual units in a mole of the crystal. The lattice energy of a unit, , denoted by U, is the energy of the unit when in the lattice of an infinite crystal and is the sum of the contributions ¢(r) , due to all surrounding units, where Mr) = 1A: - 32- r with r the distance of the surrounding units from the unit whose lattice energy is being calculated. Cohesive energy density, denoted by A , is the energy per mole of a substance that is required to remove a unit from the matrix to a postion far from its neighbors. o n I O as e .1 at- -Cu‘ 10 Let: ) Ab. Q's-o -n 3 27 Evaluation of Lattice Energy and Crystal Potential Energy Density For purposes of evaluating the crystal potential energy, we will consider polyethylene single crystals to be made up of units of (-C2H4-) (Figure 2. 2). This model will also be used later in connection with the development of interaction force constants in Section 2. 3. The lattice structure may, thus, be represented as shown below: b-axis (o. 6. 0) ck e e o ‘3’ <3 ’5 (00 4! .0) c C} \( $ \ X ’\ x. \1 yr (0: 29 0) d’ ‘3 \> D A 2 <3 (09 Os 0) Q; A J Ax} - (2.0.0) (4.0.0) (6.0.0) 3-..... Figure 2. 4. Schematic representation of two-dimensional lattice structure with lattice points occupied by. (~CZH4-) units. Letting 2.34 and :here ie 2, ever. < 2115 leis-r.- “will 5““ V tzatv The: 28 we may then write the position vector of a lattice point (i, m, n) as A .s _ A e . rlmn - Zelil + mezi2 +ne3i3 , 2.35 A where 2, m, n are integers and il, 12, i3 are unit vectors along the a, b and c axes respectively. Therefore, the distance rlmn is _ [a 2 + 2 + 211/2 rlmn ‘ °1) (Inez) (“'33) . 2.36 From Figure 2. 4 it can be seen that only when 2 and m are both even or both odd is the point occupied by a real unit. Also, all the units for which both 2 and m are zero should be excluded; they belong to a single chain and, hence, are permanently attached through the C-C bonds. It follows from 2. 26, which gives the energy of a pair of units, that we can calculate the lattice energy U of a (0, 0, 0) unit from 1 °° ' : — Z . U 2 l, m, n:-ao ¢£mn(r) 2 37 1 A B =22 (_1"2" - T" 2°38 lmn rACmn l l =-2+[2(-‘IEZ—-—6——)]B, 2.39 rZmn rafmn where from 2. 32 "U II NIH A H O V 0‘ 29 and both Land m are odd or even and n equals any integer, but 1, m,n ;/ 0. This reduces the problem to one of calculating sums of the type °° l A = Z S 2. 40 s £,m,n;-°° r1 mn for s = 12 or 6. Substituting for 2 _ 2 2 2 rlmn —(1e1) + (mez) + (ne3). from 2.36, we get A 5 1 S 1,31, n: -m [(181)2 + (mez)2 + (ne3)2] 8/2 2.41 Therefore we may write U in the form U - is( A - ) 2 42 ‘ 2 P 12 6 ' = l B A 2 43 2 12-6 ' where A12-6 = pA12 - A6 . Crystal Potential Enggy and Cohesive Enem A gram mole of a substance contains 6. 0249 x 1023 units, called Avogadro's' number and denoted by N . Let M be the molecular weight of the lattice units (-CZH4-). Therefore, M 30 grams of polyethylene will contain NA units. Thus, the crystal potential energy per mole E is E = NAU’ 2.44 where U is the lattice energy of a single unit, as determined in 2. 43. The cohesive energy density has been determined by Small (16). However, he gives values of 6, which is the square root of the cohesive energy per unit volurre;thus, 62 determines the cohesive energy per unit vdume. In order to convert this to a molar value we must determine the vdime of a mole of crystalline polyethylene. If p is the density of such material, the volume V of M grams will be V = 5’1- 2.45 p Therefore, the cohesive energy per mole, A , is A : 1:31-1- 62 ; 2. 46 and equating the values of A and E obtained in 2. 46 and 2. 44, we arrive at: A = E 2.47 M 2 T)- 6 .. NAU 2.48 But from 2.43 U E- B A 2 12-6 ’ which when substituted in 2. 48 gives -9 '6 U. 31 2M62 NApA 12-6 The expression for A then follows from 2. 31b: A pB ZRM 62 2.50 NA P A12.6 The Lennard-Jones potential constants A and B, defined by expressions 2. 49 and 2. 50 will be evaluated numerically later in Section 2. 5, by substitution of the values of several physical constants such as M, NA’ p and p, and by making use of the series summation for A12-6 developed in Appendix I. 2. 3. Interaction Constants and Elastic Constants In order to calculate continuum or macroscopic elastic constants in terms of molecular force constants, it is necessary to consider the forces of interaction that result when a lattice unit moves relative to the units which surround it. Since the force fields vary nearly linearly with distance for small displacements, the slopes of the force curves at the separation distances of the surrounding units determine the so-called interaction constants. These constants may, therefore, be obtained in terms of the intramolecular force constants (such as the C-C bond stretching or contraction, bending and repulsive force constants) and the intermolecular Lennard-Jones potential constants. In this section a connection between the elastic constants and the interaction constants of polyethylene single crystals is established 1“». Nd. 1. Av. h.“ A v 32 by following a procedure similar to von Kafrmafn's for simple cubic crystals, as discussed in Reference (14) by Kittel. Components of the net force acting on a unit are obtained by considering its inter- actions with the surrounding units up to second nearest -neighbors. These expressions, which involve finite displacements, are converted into partial differential equations by introducing the lattice parameters a, b and c, and by taking limits. Newton's law is then applied to convert the force equations into equations of motion, in order to compare these with the corresponding continuum Equations 2. 25. A comparison of the coefficients of appropriate partial derivatives in the two sets of equations yields the desired expressions for the elastic constants in terms of the interaction constants. These expressions may be modified to apply to first nearest-neighbor interactions only simply by eliminating the terms pertaining to second nearest-neighbors. Also, the central force assumption is applied in a rather limited manner to polyethylene single crystals. The C-C bonds along the chain axis have strong resistance to bending in directions normal to the chain and, thus, make the forces between units on the same chain non-central. The forces between units on different chains may, however, be treated as central. Model and Notation Consider again, as in Section 2. 2, that the lattice points are occupied by (-C2H4-) units. Figures 2. 5 and 2. 6 show both the first and the second nearest-neighbors in one quadrant formed by the positive x, y and z-axes. An additional axis (x') along the diagonal of the rectangle (a, b) in the xy-plane is also shown. 33 Y (0.1.0) \ b (1',0,0) L C (0.0.0) a ($70.0) x (0.0.1) Figure 2. 5. First nearest-neighbors in the first quadrant only. (0.1.1) I (0.0.0. 1 '0'1 1,0,1) Z Figure 2. 6. Second nearest-neighbors in the first quadrant only. 34 If y' is considered to be in the xy-plane, normal to x', Figure 2. 7 then represents the x‘y'z set of axes. 90 Figure 2. 7. Rotation of x' y' z with respect to x y 2. Similarly, by considering x" to be along the diagonal of the rectangle (-a,b), the x"y"z set of axes is shown in Figure 2. 8. xII y b -a X YII Figure 2. 8. Rotation of x" y" z with respect to x y z. 1 m a N“ C‘.) I“w 4.“ ‘_ 35 Considering a, b, c and -:—~/a2 + b2 as units of distances along the respective axes x, y, z, x' and x", the lattice points may be labelled by their (3, m, n) coordinates, 2, m and n being integers. Thus, the points listed below indicate first nearest-neighbors: (l, 0, 0), (-l, 0, 0);(0, l,0)‘,.(0,-1, 0);(0, 0,1),(0, 0, -l);(1', 0, 0), (-l ', 0, 0) and (1",0,0),(-l",0,0) 2.51 Only four of the first ten nearest-neighbors are shown in figure 2.5. It may be observed that nearest-neighbors, as defined here, are not equidistant from the central unit (0, 0, 0). This is due to the geometry of the orthorhombic cell, for which the three parameters a, b and c are inherently unequal. An additional feature peculiar to the poly- ethylene lattice structure is that units corresponding to (1 ‘, 0, 0) and (1", 0, 0), along the x' and x"-axes respectively, are considered to be first nearest-neighbors. Similarly, the points (0,1,1),(0, -l, 1),(0, 1, -l), (0, -l, -l); (l, 0,1),(-l, 0,1),(1, 0, -l), (-1, 0, -1); (1', 0,1),(-1', 0,1),(1', 0, -1), (-l', 0, -l) and (1”, 0,1),(-1", 0,1), (1", 0, -l), (-l ", 0, -l) 2. 52 are the second nearest-neighbors. These are sixteen in number; however, only three are shown in Figure 2. 6, in addition to the four first nearest-neighbors. It should be noted that the units corresponding to (1,1, 0) are excluded because units corresponding to (1', 0, 0) and (1 ", 0, 0) lie between these and the central unit (0, 0, 0). Equations of Motion Let Fx’ Fy and F2 be the components of the force on the unit (0, 0,0)along the axes x, y and 2, respectively. Similarly, the :- no ‘5‘) 36 displacement components of the unit at (l, m, n) may be represented by utmn' v‘mn and wlmn . Interaction constants will'be different for different units and will also depend upon the direction of the displacement. Defining kliii’nn as the force on the unit (0, 0, 0) along the x1 -axis per unit displacement uj of the unit (I, m, n), where i,j = 1,2,3 and x1, x2, x3 correspond to x, yand 2 while ul, u2 and 113 correspond to u, v and w, respectively, the interaction force components Fx’ Fy and F2 are derived below: _ k11 11 Fx ' k100(‘1100 + “-100 ' zuooo) + k010(“010 + ULo-lo ' 2‘1000) k11 ”001(“001 + u00-1 ‘4me + k1'100H‘11'00 “-1'00 ' “000) 11 + (“1"00 + u-l"00 ' “000” + k101[ (‘1101 + “-10-1 " 211000) +(u +u -2u )]+k13[(w +w -2w ) -101 10—1 000 101 101 10-1 000 -(w +w )]+k“[(u +u -2u ) -101 10-1 W000 011 011 0-1-1 000 + (1.101”1 + uO-ll - 2u000)] 2.53 +k1'01{[(“l'01+“'.1'0-12‘1000) ”‘1 1'01 +111'0..1 ' zuooon +[(“1“01 +“-1”o-12uooo) ”‘1 1"01 +ul"0-l " zuooon} +k1?01{[(w1'01+W-1'0-1 ‘ zwooo) ' (“V—1'01 + v".1'0-1 ' zwooon +[(w1“01 + v"--1"o.-1 ' zwooo) " (W-l”01 +W1"0-1 zwoo’om +k k1'01{[ ("1'01”r v-1'0-1 ' 2v000) ' (V—1'01 + Y-1'0—1 ‘ zvooo” +[(""1"01 + V-..1"0.1 ' 2v000) ‘ (V-1”01 +Vinc-.1 ' “000’” ° 37 Expressing (ulmn +u-l-m-n' 2u u000)’ for example, as (ulmn ), we may rewrite 2.53 in the form F -k (E )+k (E )+k“(E ) x 100 100 010 010 001 001 11 - — + k1'00[ (“1'00) + (Elnoofl + k101[(u101) + “1.101“ 101[ (W101) (‘V 101)] +k011[ (“011) + (301.1“ +k kl}01{[(u1'01) +(u .1'01):I +[(u11101) +(u _11101)]} + kl3'01{[(wl'01) ($.1'01 )] +[(-‘;1I101) ’ (13111101111 ‘1' k11201{[(V1101) " (V _1101)] +[(V1”01)-(V_1"01)]} , 2.54 which involves the following ten interaction constants: 11 11 11 11 11 13 11 11 13 12 k100’ k010' k001' kl'OO’ k101’ k101' k011’ k1'01' k1'01 and k1'01 2,55 The component of force FY may be written as 22 — Fy ‘ k100(V10 k22 k1'00[ (Vl'OO) + (v1..00)] + k011[ (V011) + (V01 1)] 22 o)+k 010(V010’ + 1‘ 001(V001) + +k01l“W 011) ' (EV—01-1)] + kl'201{[(vl'01) +(V .1'01):l +[(v1'”bl)'+ (:1; _11101)]} + k1I01{[(u1101) " (11 -1101” +[(u11101) "‘ (‘3 _11101)]} 2 -— _ , _. +k1'301{[(w1'01) (w-l'01)] +[(W1"01) -(w-l”01)] o 2.56 which involves the nine following interaction constants: 22 22 22 22 22 23 22 21 23 k100’ k010' k001’ k1'00’ k011' k011' k1'01' k1'01 and k1'01 2.57 38 And, similarly, the component of force Fz is 33 — 33 —- 33 Fz z klooIWloo) + k010IW010) + k001IW001 ) +1'00[IW1'00)+IW1“00)] +1‘101IIW101HIW101’I k101II“101) I“ “-101” +k011IIW 011)+IW01-1)] 321IIV011) ' IV01 -1” “‘1'301IIIW 1'01) +IW-1"01)] +[(3v'1..01) +IW-lH01)” +k1'01IIIV1'01)'IV-.1'01)] +IIV1"01)'IV1“01)]} +kl'01{[(u 1'01 )u-( -1'01)] +[Iqu1HOl) ’Iu_11101)l} b 2-58 involving the eleven following interaction constants: 33 33 33 33 33 31 33 32 33 100' k010' k001' k1'00' k101' k101’ k011' k011' k1'01' 32 31 k1'01 an“ k1'01 k 2. 59 Thus, the total number of interaction constants involved in all three force equations is 10+9+11 = 30 . Dividing through by the respective lattice distances and taking limits, the above difference equations 2. 53-59 can be converted into the partial differential equations given below: F =aLk11 282u +kll b2 azu +k11 C2 82u +k11 42.4.2 x 100aL "'2' 010 “"7 001'"'2 1'00“?" 8}: By 82 82u + 8Zu +k kll (a2 + 2) 8Zu + 8Zu Z a Z 101 ° “'2' "Z ax12 x21 8x13 3"31 2 2 2 2 13 2 2 a w a w 11 z 2 a u a u +k101 (a +C) a -3 +k011(b +C) $7 + E2 1"13 x31 x23 32 +k11 (34132443) 2u + 8211 + azu + azu 1'01 4 a 2 a 2 ”'8 ‘2 _ 3"" 2' x1'3 x311 3:1,,3 "31" 13 a2+bz+4c2\ 82w 32w 32w 82w + k . ( , —-—— - —— + —— - ——- 1 01 4 a 2 a 2 a 2 a 2 "13 x31' x1..3 x31H + k12 (a2+b2+4c2\ 82v _ 32v + 2v _ 32v 1'01 4. I “—3 2 —a 2 “—3 2 "8'2 x1'3 x311 x1"3 x31H 2.60 2 2 2 __22 26v 22 28v 22 28v “klooa ‘7“‘010" —'Z'+koo1° 2 3x 3y 6 +k22 (az+b2) 32v + 82v +k22 (132+ 2) 2v + 32v 100 4 78x "—3 2 011 “—3 2 —a 2 12 x21 "23 x32 2 2 + k23 (b2+C2) a w _ a w 011 '“'—'3 2 —a 2 x23 "32 +k22 (a24b2+4c2) 32v + 32v + 32v + 32v 1'01 4 a 2 a 2 a Z a 2 ‘ x1'3 x31' x1"3 "31'I + k21 (az+bz'-l-4cz\ azu 8211 + an 3211 1'01 4 ‘ ' ‘8“2' ' ”'3 2 “a 2 ' ‘73 x1'3 x31' x1..3_ x31" 23 az+b2+4c2\ 82w 82w I 82w 82w +k ( 1 , - — + - -——-— 1'01 4 a 2 a 2 a 2 a 2 "1'3 "31' x1"3 x31" 8x 3y 8z + k33 (a2+b2) 32w + 32w + k33 (212+ 2) 82w + 82w 1'00 4 a '8'"? 101 a a 2 x12 x21 "13 x31 2 2 2 2 31 2 2 3 u 8 u 33 2 2 8 w 8 w +k101( + ) 73 - :2) +k011(b+ )(—7-8 + —-—ax2) x13 "31 "23 32 2 2 32 2 2 a v a v +k011(b +c) —2-8 --——-32) "23 x32 + k33 a2+b2+4c2\ 32w 32w 32w 32w , ( , + + + 1 01 4 a ‘73 a a x1'3 x31' x1H3 ”‘31" + R31 3211 8211 +. 3211 8211 1'01 "“8 2 " —a 2 ‘"'2'8 ' ‘78 x1'3 "31' x1"3 "31'H + k32 32v _ 32v I + 2v _ 62v 1 '01 '8' 2 "a "2 “'3 2 "a '2' "1'3 x31' "11'3 x31" 2. 62 Here, the xij diagonal axes lie I in the xixj -plane, where i,j = l, 2, 3,1' and l", such that x1,3 is the diagonal axis along the rectangle (%~j'az + b2, c) in the x'z-plane. These axes are shown in Figure 2. 9 a-e below: v y Y X b a a a a x x31 z Z (a) (b) y Y b b -a a X x C x1"3 x1'3 c Z x31' z x31” (d) (e) Figure 2. 9. Geometrical representation of axes xij (a) xl‘2 and x21 (b) x13 and x31 (c) x23 and x32 ((1) x1,3 and x31, (e) 3:1,,3 and x31” . 42 Transforming partial derivatives with respect to the x. .'8 into partial derivatives with respect to x, y and z in Equations 2.60 -62, by utilizing the transformations derived in Appendix II, these equations bec ome: F =k11 2 3Zu 11 2 32u 11 2 32 u x 1002‘ 2 +k010b ' Z “‘001 C ""2 3x 3y 32 2 2 2 2 111 23u 23u 11 23.u 23u +‘2'k1'00 a‘7+b"2 +2k101a‘7VC‘7 3x 3y 3 32 2 2 2 13 aw 11 23u 23u +k101ac5—-5—x z +2k011 b ‘76 +c -—2-) y 32 2 2 2 11 23u 23u 2 3n “(1,01 a——z—+b—-2-+4c 7 3x 3y 3z +4kl3 bc i!- +4k12 b 33-3?— 2 63 1'01 3x32 101 ° 3y32 ' _k22 a2 32v +k22 b2 32v +k22 232v y" 100 '3 2 010 "2 001c "2’ x 3y 32 2 2 2 2 122 23v 23v 22 23v 23v +2 kl'OO 7 +1) ——2- +2k011 b 7 +C "'7 3x 3y 3y 32 2 2 2 2 23 3w 22 23v 23v 23v +4k011bc 3y32 +kl'01 a -—7 +b -—-2- +4c —-2- 3x 3y 3z 2 2 21 3u 23 3w + 4k1,01bc m + 4k1,01bc m; 2. 64 3x 32 2 2 2 2 l 33 2 3 w 2 3 w 33 2 3 w 2 3 w +2-k1,00 a—z- +b -—-2— +2k101 a——2-+c -—-2- 3x 3y 3x 32 2 2 2 2 31 3 u 2 3 w 2 3 w 32 3 v + 4k101 ac m + ZkOll (b ~78}, + c .782 ) + 4ko11 bc WY 2 + k33 a2 32 w + b2 32w + 4C2 2w + 4k31 bc 3zu 1'01 “:2 70y “‘2: 1'01 W + 4k3 bc 32" 2 65 1'01 532 ' By collecting coefficients of the various partial derivatives, the above equations may be rewritten as: _ 2 11 1 11 11 11 32u 11 1 11 11 Fx’ 3 Ik100 V2k1'00 V Zk101 V k1'01) "2 V b P‘VIV‘010 21‘1'00 V 2k011 k )32u+c2.(k11-+2k11 +Zk11 ) 31.12 +4 k13 32w 1'01 WY 2 .. . 001' 101 011V 4k1'01 “‘2 ac 1012—52 2 2 13 3w 12 3v +4bckl,01-5—5-z— +4bckl,01W 2.66 F _a2(k22 +11(22 +1: k22 ) 3v2 +b 2(k22 1k22 +2132 +k )3zv y” 100 2' 1'00 1'01 “'2 010 2 1'00 011 1'01 ”28), 2(k22 +21<’22 +4 kzz ) 32" +4b C(kz +)1<23 82W +c 001 011k1'01 “—2 011V 1'01 W 2 21 3 u +4bckl,01 W 2.67 44 2 _ 2 33 1 33 33 33 3w Fz‘a Ik100V2k1'00V2k101Vk1'01V‘a'x'2 +1320(33 +1193 +2193 +k33 ) 32w 010 2 1100 011 1101 “'73), 2 33 33 33 33 32w +c (1:001 + 2 k101+2 k011+4k1,01)—-2—az 2 2 2 31 3u 31 3u 32 32 3 v V4a°k101 '“ax'Tz V4b° k1'01 —3y3"z“ V4b C Iko11 +kl'01)3y3z 2.68 Newton's law for the force components in the directions x, y and 2 may, of course, be written as F _3.‘._ = {3 abc p .5; ~ abc = p v and Fz O. m- = p W Z. 69 where abc = volume of a unit cell. The corresponding continuum equations 2. 25 based on the generalized Hooke's law are relisted below to facilitate comparison: " - 32“ + La“ + 32“ +( + )fi-H +C )Wazw P u - C11“? C66 2 C55' '2 c12 C66 axay C13 55 x z ax By 82 2 2 2 Z 2 ,, _ 3 v 3 V 3_V 3 u 3 w PV - C663? ”2287 V C44 022 + (°12+°66’5§75§VI°23 ”44V 5W 32 32w 2 3 2 .. _ w 3 w 3 u 3 v pw -c55 73x +c44—2-ay +C33_Taz +(c13+c55)-5--5--x z +IC23+C44)3__—y3z 45 Comparing coefficients in the two sets of equations we obtain the following expressions for the elastic constants the interaction constants kg'nn : a 11 1 11 11 c.. in terms of 1J 11 C11: "152' Ik100 V2 k1'00 V 2 k101 V k1'01’ C66= EPEIV‘310V2V‘1100V21‘311VkiIm) 2'70 C55 z 3%Ik31111 V 2 k131V 2 1‘31 V 4 ki'lm) 612 V C66 ._. 0 C13 V °55 =1? kigl C66 = EVE “130 V2 kIgloo V kV3201) C22 = ab: Ikgfo V2 k177200 V 2 1‘31} V k173201) 2' 71 C44 z 396' “(2131 V 2 kgfl V 4 ki'zm) C12 V C66 ‘ 0 C23 V c44 = 21V Ik(21:11 V k13301) 655 = BEE Ikigo V 2 k1'300 V Z k11311 V k11301) C44 = '33 “((3110 V '2' k1,1300 V 2 kgil V @301) 2'72 c:33 = 2913 “‘331 V Z 16131 V Z kgil V 4 k1?01) C13 V C55 = “E k15:11 C23 V C44 '"' g “(3111 V k$01) 46 These in turn may be combined and rewritten to give: a 11 l 11 11 11 C11: 13'; Ik100 V2 k1'00 V 2 k101 V k1'01’ (‘22 :29; ”‘ng V2 k1'200 V Z kgfl V R3201) c33 '“' 5303531 V 2 k1:31 V 2 kgil V 4 k1?01’ C44 = 2% Ikcznzn V 2 1‘31} V 4 kf'zm) °r C:44 = 2% Ikgio V2 k1:300 V 2 1‘31 V kfiol) C55 = 3913' “(31111 V 2 k131 V Z k311 V 4 R1101) or C55 2 fi— (kigo +é- kfim + 2 #1531 + kffbl) 2.73 c66 = 21% “(310 V2 k1100 V 7' k311 V ki'lm) °r C66 '"' Ba? “(ff-10 V2 k11200 V kf'zm) C12 ._. ' c66 c = 5- kl3 - c 13 b 101 55 = g kfln ' c55 C23 '“' g Ikgil V k1.1301) ' c44 = '3’ “3011 V k103201) “' c44 The exPressions 2. 73 may be simplified by excluding the terms involving the second nearest neighbor interactions; this yields the following expressions for first nearest-neighbor interactions: 47 _ __ 11 _1_ 11 C ’ Ik100V2 k1'00) b 22 1 22 C22 = 5‘6 Ik010 V 2 k1'00) C33 : 2% k313n c44 : 3% kgfn‘r: 2% Ikgio V2 k'1'300) 2' 74 C55 = 5% 1‘33““ 6% Ikigo V'12 k:1'300) __1_3_11111=_a_1_22_1_22 C66 ‘ ac Ik010 V 2 1‘1'00’0'r bc Ik100 V 2 R1100) C12: ’C66 °13= ‘°55 C23= “C44 Constants C44, c55 and c66,-:and correspondingly C12’ on and C23 are double-valued. An appropriate single numerical value will be selected fori'thes'e; later in Section 2. 5. Central Force Assumption If only central forces are allowed, the following sixteen of the thirty interaction constants entering Equations 2. 54-59 vanish: 11 13 11 13 12- 22 23 .21: 23 k010' k101' k011' k1'01' k101' k100' k011i" k17.'01i"k1'01' 33 33 33 31 32 32 31 , k100' k010' k1'00' k101' k011' k1'01' k1'01 ' 2'75 while the following fourteen will still be involved: 48 kiéo’ k331' ki'loo' k11111: ki'lor k310' k331' kf'zoo' kgfl’ ki'zov @361: 1‘31: kgil’ k11,01 2°76 It may be noted that, unlike nonpolymeric crystals, the constants kg?” and kggl do not vanish because of the bending resistance of the C-C bonds. This means that the central force assumption is being applied in a limited manner. The expressions for the elastic constants cij under this central force assumption, including interactions up to second nearest-neighbors, become: C11 ' biIk130 V'12k1I00 V 2 k131V R1101) C22 = 5% “((2)10 V l21‘12‘1200 V 2 R311 V #1201) C33 V ab ”‘331 V Z kigl V 2k311 V “$01) c44 = 3'1? “331 V 2 1‘31 V 4 kf'zm) °r c44 = 3136 I2 kgil V 1615.301) C55:;%(k(l):)l+2k1:11+4k1'101 2.77 °r C55 z Bi— IZ kigl V kfim) C66 : 5% I2 k1100 V kiI01) °r C66 = BEE-(1: kf'zoo V kf'zm) C12 = ‘ C66 Magmtudes of c23, c13, c12 are equal to those of C44, c55, C66 due to drOpping the interaction constants for the central force assumption. This does not imply that the number of independent elastic constants is reduced to six. 49 =-c c13 55 C23 " C44 But for first neighbors only these may be further simplified to give: a 11 1 11 C11“ 3? Ik100 V2 k1'00) b 22 1 22 c=22 : E'e' Ik010 V2 k1'00) C33 = 2% k3031 C44: 29b" kgfn °r °44=°' :__g_:__ kll ab 001 °r C55:0 1 .19.. k11 1 22 __ ..__§_ °66‘2 ac 1'00°r“'2 bc k1'00 2'78 c:12 “' 'C66 C13 - 'C55 C23 = '°44 These show that polyethylene single crystals possess shear resistance even when first nearest—neighbor interactions and central forces are assumed. It may also be remarked that identical expressions are obtained for first nearest-neighbors from strain energy consider- ations, as shown in Appendix III. 50 2. 4. Interaction Constants and Molecular Force Constants The elastic constants were related to the interaction constants in the last section, and in Section 2. 2 it was explained that interaction forces result directly from relative motions of the lattice units in the intramolecular and intermolecular force fields. The objective of the present section is to obtain expressions for the interaction constants in terms both of the intramolecular force constants, such as those for C-C bond stretching, bending and repulsion, and the intermolecular force constants, such as those appearing in the Lennard-J ones potential. It is assumed as before that the weak secondary bond forces between units lying on different chains are central. However, the same cannot be said of the forces between units lying along a single chain; these are due to the strong connecting C-C bonds which provide resistance to bending in lateral directions. For this reason the central force assumption is limited to intermolecular forces only. The following interaction constants, 11 100’ 11 ll 11 ll _ 22 22 001' k1'00' k101’ k1'01’ k k k 010’ 001 k 22 22 22 33 33 33 33 k k k k101' k011' k1'01 k1'00’ 011' 1'01' 001' will be obtained in terms of the molecular force constants such as the C-C bond stretching, bending and repulsion force constants K, H and F, respectively, and the Lennard-J ones potential constants A and B. The rest of the interaction constants (listed in 2. 75-) vanish under the limited type of central forces that exist between the lattice units, as . discussed in the preceding paragraph. 51 Constants Along the Chain Of the fourteen interaction constants needed for interactions up to second nearest-neighbors under the central force assumption, three are for forces between units along the same chain, viz. , 11 k22 and k33 k001' 001‘ 001 ° These will primarily involve the C-C bond constants. Further, if displacements remain small and the planar zigzag conformation of the polyethylene chain does not change, it may be assumed that no torsion takes place; and any deformation may be accomplished merely by stretching and bending the C-C bond. Thus, if as in Figure 2.10, 6r = change in the bond length r 60. = change in the bond angle a/Z and 6d ll change in the distance Vii-between two alternate C-atoms, r a/Z o/Z r C Figure 2.10. Geometry of two corresponding C-C bonds showing the bond length r, bond angle a and the distance between alternate C atoms. 52 the strain energy V becomes In—n V = 2[%2-K(6r)2 + 2 H (r6c1)z - :12— F(6d)2] 2.79 where K, H and F represent the stretching, bending and repulsive force constants. . . . ll 22 To determine the interaction constants k001’ k001 and kggl, particular expressions for V must be derived by considering the respective deformations in the x, y and z —directions; these are illustrated below: Z K\ \\\ \\\\ 6r”): 0 ‘1’ I 62 54 44' ““1 ' 1 r / : o / 1 ‘”’ Y 0 : ”’4:\ p l 0 K 59 5 \ 41° ' / Y \ ' I 4 <64, 1' x \ IV 6x ' I p\\ 1 /I 4> 2\__-:._J’ x I \‘\ '”6X _’->1 .6}, (a) (b) Figure 2.11. Deformation of C-C bonds (a) in a general direction (b) in x-direction.only. 53 z e I . 343 54> V / ¢ VI / \ \\ 69/ " 423:3 V 1/2 53* / 54°44' X (C) (d) Figure 2.11. Deformation of C-C bonds (c) in y-direction‘only' (d) in z-d'irec't'ion only. ’ ' ° -- 1 . . 11 001 The Constant k By definition, kggl is the force on the unit (0, 0, 0), per unit displacement u of the unit (0, O, l). Denoting this displacement by 6x, as inFigure 2.11 (b), the quantities Br, 60. and 6d of Equation 2. 78 may be obtained in the following way. Letting cs ll N|=1 l le where 921 = 54044', -410 49 . .9. ll N|=I [\- pl 54 The bond length r is given by r2=x2'+y2+z2 ; and differentiating this expression we get 2r 6r 2x 6x + 2y by + 22 6z, 11 where for R001 , 6y = 6z 2 0 . Therefore, 2r 6r 2x 6x 01' Gr = 6x Hlx Now, since p = r cos ((1/2), as shown in Figure 2. 11(a), x E cos (b r c1 0. a. . o. — = = - cos — cos = cos — 6.05 = cos -- 811'! 4.1 r r r 2 IV) 2 (I) 2 ’7 and we have 6r = cos % sin 410 6x = cos 54. 7° sin 41° 6x = g 6x , where g = cos 54.7o sin 410 . Also, from Figure 2.11 (b) we have 0 69 =£9_§—riL 6x Hlo. 5x, 55 where d = cos 41° and 6d = 0 . Consequently, substitution for 6r, 66 or 60., and 6d in 2. 79 yields V = K(g 6x)2+ H(d 6x)2 ; 2.80 and differentiating this with respect to 6x, we get an expression for F : x _ dV _ 2 2 Fx— '“‘—d6): — -(2gK+2dH)6x 2.81 Therefore, kcl)31 , being the force per unit displacement, is given by F 11 _ x _ _ 2 2 The negative sign indicates attraction for positive displacement. 22 The Constant kOOl Following a procedure similar to the above for 1:331, but considering only the displacement 6y, analogous expressions for 22 . k001 may be obtained: 2 2 V = K(h6y) +I-I(e6y) , 2. 83 h = cos 54.70 cos 410 e = sin 410 56 _ dV_ 2 2 Fy—-d6y—-(2h K+2e H)6y 2.84 22 _ 2 2 1.001- 2(hK+e H) 2.85 33 The Constant k001 Similarly, by considering only the displacement 62, the corresponding expressions for R301 can be derived: v = K(iéz)?‘ + H(f6z)2 - 1:782)Z , 2.86 1 = sin 54.70 f = cos 54.70 . .2 2 Fzz-(21K+2fH- F)6z 2.87 33 __ .2 2 1:001 —2(1K+fH-ZF) 2.88 Other. constants are essentially derived from the Lennard-Jones 6-12 potential curve (r) shown in Figure 2.3. This defines the force existing between the lattice units and its variation with separation distance as well. If the latter is less than the equilibrium distance r , the force will be repulsive and if it is greater than the equilibrium distance, it will be attractive. For the small displacements with which we are concerned, the force may be assumed to vary linearly, though the rate of variation will evidently be different for different separation distances. Such an assumption makes it possible to evaluate the inter- action constants by determining the slope of the force curve at the various lattice distances. Thus, if F(r) is given by F(r) = If? .. 9% , 2.28 r r then the derivative of F(r) with respect to r is dF _ 156A 42B :1"; — --;—i-Z- '1' :‘g— . 2.89 This determines the interaction constants for the first nearest-neighbors 8.8 11 _ dF _ _. 156A 4213 k100 ‘ " IE?) ' 14 " 8 2‘90 1‘38. a a and 22 _ dF _ 156A 4213 k01o - ‘ (a?) - ‘74" - T ' 2°91 r=b b b The interaction constants for the diagonal units and second nearest - neighbors are determined from the components of the diagonal force, or the force along the line joining the central unit with the surrounding units . Thus, 11 __d__ a 12A 6B 1'00 dr ,1 . 13 7 ‘ [3.2+ b2 r r r _ 1 2 2 " 2- a + 1) giving: k11 _ a 156A , 4213 2 92 1'00 — 2 2 7 '- 2 2 4 ° 2 2 a +b . ,a +b 3. + b 4 _ ___._4 k22 _ b. . 156A ___4_2_8__ ' — . - V 00 2+b2 (a2+b2)7 a2+b2 4 a 4 4 k11 ___ a . 156A 428 101 az+e2 a2 + C2)? (a2 +? 4 k33 __ c . 156A 428 101 ‘ ' ' 2 2 7 ' 2 2 4 Ia2+c2 (a + c ’ (a + c ) k22 _ b . 156A 428 011 ‘ — - 2 2 7 —'—‘2“2 4 /b2+C2 (b v+c ) {b +e ) k33 = c 156A 428 011 b2+cz (b +62)? (b2+C2)4 k11 _ a 156A 428 1'01“ 2 2 2 7 " 2 2 2 4 fi2+b2+4e2 a +b +4e \ a +b +4c 4 I 4 k22 _ b 456A . 428 1'01 ‘ 2 2 2'7" ‘ 2 2 2 4 [a2+b2+4cz (a +b +4c \ (a +b +4e I 4 I 4 I k33 _ 2e f 156A 4 428 1101’ 2 2 42 7 ' 2 2 24 J3. +102 + 4C2 (a +b4+4c ) (a +b 4+4e } 2. 94 2.95 2. 96 2. 97 2. 98 2. 99 2.100 59 Numerical values of the interaction constants will be obtained along with the other constants in the next section (2. 5), by substituting the values of the intermolecular force constants A and B and the intramolecular force constants K, H and F. 2. 5. Numerical Values of Constants Expressions for the Lennard-Jones potential constants were derived in Section 2. 2, while in Section 2. 4 expressions for the inter- action constants were obtained in terms of the C-C bond stretching, bending and repulsive force constants and geometric parameters such as bond length, bond angle, lattice distances and setting angle. The connection between the elastic constants and the interaction constants was established in Section 2. 3. In the present section, numerical values for all of these constants are obtained: first the Lennard-Jones constants, secondly, the interaction constants, and lastly, the elastic c onstants. Lennard-Jones Constants In Section 2. 2, the expressions for the Lennard-Jones potential constants A and B, 2.49 and 2.50, B: 2M 62 NAPAIZ-é 2 2pM6 Azsz , N pAlZ-é involve various quantities to which numerical values may now be assigned. The molecular weight M of the (-CZH4-) lattice units is: 60 M = 2x12+4 = 28 2.101 Avogadro's : number NA is: NA = 6.0249x10Z3 2.102 The cohesive energy density 62 for polyethylene, determined experimentally by Small (1 6), is: 62 = 62 cal/cm3 2.103 .. 9 3 — 2. 595320 x 10 erg/cm 2. 595320 x 10'15 erg/A3 The density p of crystalline polyethylene . varies from one manufacturer to another; however, the variation is small and one representative value, listed in the commercial bulletin of the Dow Chemical Company, Midland, Michigan (27), is: 3 g . p = 0.964 gram/cm 2.104 The factor A = p A - A6 has been evaluated in Appendix I; 12-6 12 its value is: _ -3 -6 - 12-6 - 2.345833 x10 A I-35 The factor p = %- (r0)6 has also been evaluated in Appendix I: p = 3. 897619 x103 A6 1-34 Substituting these values in the above expressions for B and A, yields: 61 2.177300 x10"10 erg A6 B = = 2.177300 x10.58 erg cm6 2.105 A = 8. 486677 x 10'7 erg A12 = 8.486677 x10"103 erg cm12 2.106 Interaction Constants In Section 2. 4 the interaction constants kiifjmn have been divided into two categories: (a) Interaction constants for units on the same chain. (b) Interaction constants for units on different chains. These are evaluated below. (a) Expressions for constants in category (a) are derived in Section 2. 4. These relations (2. 82, 85 and 88) involve the C-C bond stretching, bending and repulsive force constants K, H and F which are given by Shimanouchi, et al (17): K 4. 0 3:10-3 dyne/A H 0.113e10"3 dyne/A 2.107 0. 96 x10"3 dyne/A The geometric factors g, h, i, d, e and f, are defined in Section 2. 4 in terms of the following (10,11): C-C bond length r = 1.54-A c-c bond angle a = 109° 28' 2.108 setting angle 8 = 41° Substituting these values of r, 0., (3,. we obtain: 62 g2 = 0.143724 b‘2 = 0.190197 i2 = 0.666084 2.109 d2 = 0.569587 e2 = 0.430414 f2 = 0.333922 The interaction constants in category (a) thus turn out to be: k“ = 1.275102 x 10"3 dyne/A 001 22 -3 kOOl = 1.616266x10 dyne/A 2.110 13531 = 3.482134x10"3 dyne/A (b) The expressions for the constants in category (b) are given in Section 2. 4 (2. 90-2.100). Their numerical values may be obtained by substituting the values of the Lennard-J ones constants A and B from 2.105 and 2.106 and the lattice parameters a, b and c d 7. 41A, 4. 94A and 2. 55A. The result is: kito = - 9.180603 x 10‘8 dyne/A kzz = - 1.371359 x 10"8 dyne/A 010 k11 _ 4 -6 1,00- ..219081x10 dyne/A 1.12:200 = 2. 809002 x 10"6 dyne/A 11 -8 k101 = - 6. 075525 x10 dyne/A kg?” = - 2. 090739 x10"8 dyne/A 1.22 - 4. 538807 x 10'7 dyne/A 011 63 33 011 11 1'01 - 22 1'01 - 33 1'01 _ 2. 342901 x10-7‘dyne/A W 1 2.843103 x 10“7 dyne/A W I I 1. 895375 x10"7 dyne/A W I I 1.956759 x 10'7 dyne/A W I I 2.111 Elastic Constants The expressions 2. 77 for the elastic constants cij in terms of the interaction constants kIVI-nn and the lattice parameters a, b and c under the central force assumption as derived in Section 2. 4, on substitution of the numerical values from above, yield the following values, including second nearest-neighbor interactions: ell = 0.948127 11:10-6 dyne/Az -6 2 €22 = 0.288779x10 dyne/A -4 2 e33 = 2.422665x10 dyne/A — 1 123761 10'4d /14.2 - - C44 - o X Yne - C23 - 0 886595x10“48 e/AZ = -c C55 " ° Y“ 13 - - 6 515515x10“7d ’/A‘Z =-e - c:66 ‘ ' V” 12 2.112 The corresponding expressions 2.73 for first neighbors only yield: e11 = 1.186831x10“6 dyne/AZ -6 2 e22 = 0.363552x10 dyne/A -4 2 e = 2.423565x10 dyne/A 33 64 1.124921 x 10'4 dyne/AZ = - c C44 = 23 - 0 887471 10"4 d /A2 — c55 - . x yne - - cl3 c _ 7 006943 3410-7 d ne/AZ = - c 66 ° Y 12 2.113 As observed earlier, the constants C44, CSS, (:66, C12’ €23 and C13 are doubled-valued. However, the constants C44 and C55 should have much higher values than the constant C66, because the former two involve movements of units belonging to the same chain. Thus, only the higher values of C44 and c55 are used; but in the case of C66, for which the two values are of the same order of magnitude, the average value is taken. Substituting the values of cij 2. 17-19 yields: E1 = 0. 377123 1410-6 dyne/Az -6 2 E2 = 0.266161 x 10 dyne/A -4 2 E3 = 2.388100 x 10 dyne/A 2. 114 All the numerical values are given to six decimal places as a matter of calculational convenience only. These may be rounded off to three decimal places for future use without any loss of accuracy. III. DISCUSSIONS OF RESULTS 3.1. Anisotropy of Polyethylene Single Crystals Anisotropy of polyethylene single crystals is a compound effect depending on the inherent nature of the lattice structure and the directional molecular forces of different strengths that exist along the three lattice axes. The complex orthorhombic lattice of poly- ethylene (Figure l. 6), consisting of (-C2H4-) as the lattice units. has been converted into a simple orthorhombic lattice (Figure 2.1) by choosing. as a basis, the pair consisting of dains at the mid-point and the corner of the rectangle (a, b). An orthorhombic lattice structure has nine independent elastic constants cij’ whereas cubic crystals have only three such constants. Thus, an orthorhombic lattice, by itself, is anisotropic in a manner which is more complex than the cubic lattice; and the situation is further complicated by the directional molecular forces that exist between the units themselves. However, this complexity has been reduced by approaching the problem from the continuum and the discontinuum points of view independently, then relating the results. 3. 2. Continuum Theory of the Orthorhombic Lattice Crystals having an orthorhombic lattice, irrespective of what the molecular forces are, would be expected to have different elastic moduli along the “three lattice axes because of the inequality of the lattice parameters a, b and c. Thus, there are three Young's moduli and three shear moduli for such crystals; however, Poisson's ratios are six in number,because e. ._ _l _ vij — ' e. ’4 J II V 65 66 A uniaxial tensile stress along the a-axis would cause a certain contraction along the b or c-axis, and this would be different from the one caused along the a-axis by a uniaxial stress in the b or c- directions. Expressions 2. 17-19, for E E2 and E in terms of Cij’ 1’ 3 have a common numerator but different denominators. Hence the expression 2. 20, which relates all three Young's moduli, can be derived. The shear moduli (323, G13 and (312 are equal to C44, c55, C66 respectively (2.11) due to the definition of the shear strains (2. 5). Expressions 2.16, 2.16a for the six Poisson's ratios must be obtained in pairs by considering uniaxial stresses along the three axes each time, and by solving the resulting equations simultaneously. The equations of motion, 2. 25, and the expression for the strain energy, 2. 22, are slightly more involved than the corresponding equations and expression for cubic crystals. The strain energy relation is only an approximation, because higher-order terms involving rotational or torsional and coupled deformations are neglected. This is the case for cubic crystals too. It should be pointed out again that the constants cij differ, not only due to the inequality of the lattice parameters, but also due to the inequality of the molecular forces in various directions. This is discussed in more detail later when their relationship with the interaction constants is explained. 67 3. 3. Molecular Forces Both intramolecular and intermolecular forces are highly directional. The intramolecular or primary bond forces which exist along the molecular chain axis are due to the covalent C-C bonds. These are several times stronger than the intermolecular or the secondary bond forces existing between the chains. The latter are a net result of the London dispersion forces of attraction and the repulsive forces caused by the overlap of the electron clouds surround- ing the nuclei. In fact, the intramolecular forces are so strong that to some extent they dominate the inherent anisotropy of the orthor- hombic lattice. Molecular chains take a planar zigzag configuration, when in a lattice; thereby preventing free rotation of the segments of the molecules about the C-C bonds. This gives the chains a definite resistance to deformation along the c-axis, which is also the chain axis, and to bending in the lateral directions a and b. The strength of the C-C bond for various types of deformations is fairly well known and the values of these constants are listed in Section 2. 4. The strength of the secondary bond forces is known only as a measure of the cohesive energy or the sublimation energy. These intermolecular forces have been assumed to be determined by a 6-12 Lennard-J ones potential, which involves two unknown constants. It should be noted that the value of the sublimation energy. as determined experimentally by Muller (28), is more than twice the value of the cohesive energy as determined experimentally by Small (16). However, the value of the latter quantity is more reliable; first, because it is the 68 more recent of the two and, secondly, because it is verified theoret- ically by the latter author. Accordingly, Small's cohesive energy data is employed here. Values of the Lennard-J ones potential constants A and B determined in this manner have the same order of mangitude as for solid argon. This is to be expected because the lattice energy is of the same order of magnitude (23). The intermolecular forces of polyethylene arise from the interaction between the hydrogen atoms, which are attached to the carbon atoms of the molecular chain by covalent bonds formed by sharing a pair of electrons. Thus, the valence electron of hydrogen spends most of the time in the region between the carbon and hydrogen atoms and very little time outside this region. The result is that the dispersion type of van der Waals forces, which arise from the time - varying instantaneous electron configurations, are very weak-ma condition existing in rare gases too, though for a different reason, It has been emphasized that polyethylene single crystals have an entangled-rectangular lattice structure in which the planes of the chains have two orientations. This fact is not considered in the computation of the lattice energy of a unit in an infinite matrix. How- ever, as illustrated in Appendix IV, the orientation of the chains becomes insignificant if one considers their interaction in more detail. The chains are situated in space in such a manner that for any two neighboring chains the hydrogen atoms are equidistant from each other. This determines the Lennard-Jones potential between chains; the net or effective potential for the two units has been obtained in Appendix IV. 69 A slightly different method than the usual low density gas approach (23) has been used to determine the two Lennard-Jones potential constants. By taking the equilibrium separation distance between the two nearest chains to determine the minimum in the potential curve, the ratio of the two constants is fixed. This leaves only one unknown constant, which is then determined by computing the crystal potential energy density and comparing it with the cohesive energy density. In the case of gases, the crystal potential energy or the lattice energy is first calculated from a general potential. Its value is then minimized to determine the value of the equilibrium separation in terms of the lattice energy and one unknown constant, which in turn is obtained from data for the second virial coefficient. However, this is not applicable to solids where the equilibrium separation and the separation for minimum crystal potential energy are identical. The triple inverse power series involved in computing the crystal potential energy converge very rapidly. Their values have been obtained by splitting them into component single, double, and triple series. For evaluation of the single series, standard formulae are given in reference (29) by Knopp. To compute the sums . of the double and triple series, they were terminated at a point beyond which the contribution of the terms is less than 0. 000015 for the sixth power and less than 0. 00000000024 for the twelfth power. As the units of distance along the three axes a/Z, b/Z, and c have been used; these lead to the above -mentioned series. However, it is only for points for which the integers along the a and b -axes 70 are even, that a real unit exists. This point has been taken into account in computing the sums: of the series. In order to compare the crystal potential energy with the cohesive energy, all the units belonging to the central chains are ignored. These units are attached to each other permanently and remain so even when the chains are removed a considerable distance from each other, as required in determining the cohesive energy density. 3. 4. Interaction Constants To establish a relationship between the continuum elastic constants and the molecular force constants, first and second nearest- neighbor interactions have been considered. The expressions for the force components on a central unit due to its motion relative to its neighbors, involve thirty constants for interactions up to second nearest-neighbors, while for cubic crystals there are only five such constants. If only first neighbor interactions are considered, the expressions contain eleven constants for an orthorhombic crystal, whereas only two constants are involved in the case of cubic crystals. In view of the inequality of the three lattice parameters a, b and c, all the first neighbors are not equidistant from the central unit. Such is the case for the second neighbors too. The first nearest- neighbors are the units which lie nearest to the central unit along the axes x, y, z, x' and x" in either positive or negative directions. The second nearest-neighbors are the units that form rectangles with the first neighbors and the central unit. In this manner the four units corresponding to (l, l, O) are eliminated from the family of second 71 nearest-neighbors, but the eight units corresponding to (l', 0, l) are included instead. A limited type of central force assumption has been applied to reduce the number of constants to fourteen for second nearest-neighbor interactions and seven for first nearest-neighbor interactions. The forces between the lattice units are not quite central, due to the units being rather unsymmetrical in shape. The major attractive forces arise from the hydrogen atoms which are located off the lattice points. However, because the forces between units belonging to different chains (secondary bond forces) are much smaller than the forces between units belonging to the same chain (primary bond forces), the former may be considered to be nearly central. This is what has been termed a limited type of central force assumption. The interaction constants have, therefore, been classified in two categories: (a) those for units belong to the same chain (b) those for units belonging to different chains The interaction constants of category (a) are obtained from the C-C bond stretching or contraction, bending and repulsive force constants, while those belonging to category (b) are obtained from the Lennard- J'one s 6 - 12 potential. . ll 22 ‘ 33 All three constants of the first category, k001' k001 and kOOl' are positive and approximately 103 times stronger than kI'IOO and kfg'oo, the only two positive constants of the second category. Other constants of the second category are negative, and their magnitudes are 10-100 times lower than these two. 72 - 11 22 As mentioned above, the constants kl'OO and k1,00 are 11 22 11 33 22 33 p081tive, while the constants k100’ k010’ k101’ k101’ k011, k011, 11 22 33 . . . kl'Ol’ kl'Ol and k1,01 are negative. The pOSitive constants are for units whose separation distance is smaller than that to the point where the F(r) force curve has a zero slope. This occurs at a distance of r = 4. 493 A -- slightly larger than the distance r0 = 4. 450A, at which the ¢(r) potential curve has a zero sloPe. Because the interaction constants are negative for units having a separation distance greater than r = 4.493A. it will be seen later that the inclusion of second nearest-neighbor interactions lowers the values of the elastic constants instead of raising them. 11 22 33 . 001, k001 and kOOl involve deformations of the C-C bonds and, thus, are obtained from the strain The interaction constants k energy expressions in terms of the particular type of deformation required. Identical results would be obtained if a general expression for the strain energy involving all types of C-C bond deformation were obtained. The constants could then be obtained by taking the appr0priate partial derivative, :though the expressions would be slightly more involved than the one used here. . . ll 22 ll 22 11 The interaction constants k100' 1:010, kl'OO’ kl'OO’ km”, 33 22 33 ll 22 33 . from the sloPes of the force curve at the appropriate separation distances. Of course, this amounts to approximating the force curve by straight line segments in the neighborhood of the location of the units. However, for the infinitesimal displacements we are concerned with,this assumption is well justified. 73 3. 5. Elastic Constants Expressions for the nine elastic constants cij in terms of the interaction constants kijmn have been derived in Section 2. 3. These are obtained by comparing the coefficients of the appropriate partial derivatives in the equations of motion, derived from continuum theory, and the force components equations, derived from discontinuum theory. However, some of the partial derivatives appear twice in the equations of motion. This leads to redindant expressions for the constants 044, C55 and C66 and, correspondingly, for the constants 023, 013 and 612 also. Selection of the appropriate expressions was not made until their numerical values were obtained and a comparison could be'.‘ made. The expressions for the elastic constants have been simplified by employing the central force assumption discussed above to eliminate some of the constants, and these have been further simplified for first nearest neighbor interactions. It may be pointed out that, for fir st neighbor interactions and the central force assumption,identical expressions are obtained from strain energy considerations ianppendix IV. In order to decide upon one expression for the constants C44, 055 and C66, all the expressions were first evaluated by substituting in the values of interaction constants. The constants 0'44, -c‘-55 and c'66 are identified as the shear moduli. The first two involve move- ments of the units belonging to the same chain whereas the constant C66 involves movements of units on different chains. Thus, the values of (:44 and c55 should be much higher than that of 666' 74 However, 066 has two numerical values, both of the same order of magnitude; and in the absence of any criterion for making a selection, it was decided to use an average of the two values as the true value for this constant. The two lower values of C44 and 055 compare well with this value of 066; however, their higher values are about 103 times larger. This suggests that the higher values of the constants are the right ones. As mentioned earlier, because the interaction constants are negative for all units whose separation distance is greater than 4. 493A, the numerical values of the elastic constants for second neighbor interactions are smaller than those for first neighbor inter- actions. Thus, it appears that the crystal gets weaker as one includes higher neighbor interactions, but the fact is that,as one includes inter- actions of all the surrounding units in an infinite matrix, the actual value of the constant is obtained. However, the contribution of neighbors higher than second neighbors is negligible :because as one goes to larger distance, the force curve levels off and its slope rapidly approaches a zero value. Thus, the value of the constants obtained by includingi'nteractions up to second neighbors is very close to their true value. . If only first neighbor interactions are considered, cubic crystals have no resistance to shear; it is only when second nearest- neighbor interactions are included that shear resistance is introduced. In the case of orthorhombic crystals, however, shear resistance in all directions is present even when only first neighbor interactions are considered and forces are assumed to be central. This is due to 75 the existence of a unit at the mid-point of the orthorhombic -lattice rectangle (a, b), and the restrictions imposed on the central force assumption in the direction of the chain axis. The values of the constants C11’ C22. and C33 are calculated to 6, 0.288729 x 10'6 and 2. 422.665 x 1074 dyne/AZ. be 0. 948127 x 10' The numerical value of C33 is about 100-1000 times the value of C11 and c22 which is compatible with the ratio of the order of 50 for the C-C bond dissociation energy of 83 kcal/mole (13) and the cohesive energy of 1.736 kcal/mole (16). Also the value of E3 = 2.388100 x 10-4 dyne/A2 calculated from oil. (2.10) is in good agreement with the observed value of E = 2. 6 x 10"4 dyne/A2 for oriented poly- ethylene, obtained recently by Sakarda et al. (17). Shimanouchi et a1. (17) have also calculated a value of E = 3. 4 x 10'4 dyne/Az for infinitely-long oriented polyethylene molecules, which is much higher than the experimentally-determined value. The constants C44, CS5 and C66, which are measures of the 4 4 shear moduli, have numerical values of 1.123761 x 10' , 0. 886595 x 10- and 6. 51551 5 x 10"7 dyne/AZ. No experimental value is available with which these may be compared to draw any useful conclusion. However, the values of the constants C44 and c55 are about 100 -200 times the value of the constant C66. This is reasonable because the former two involve movements of the units belonging to the same chain, and are thus connected by stronger C-C bonds. Further, the values of these moduli are lower than the corresponding E1, E2 and E3 values which is true in general for shear and Young's moduli of bulk poly- crystalline materials. IV. C ONC LUSIONS 1. The constants A and B in the 6-12 Lennard-Jones potential, ¢(r)= 12 -—%. r I‘ for forces existing between polyethylene chains in the crystal lattice are found to be A 8.48667 x10-7 erg/A12 and 1 O B 2.177360 x10- erg/A6 . They are of the same order of magnitude as those for argon, whose lattice energy is of the same order as the cohesive energy of poly- ethylene. 2. The ratio of the dissociation energy of the primary C-C bonds and the cohesive energy of the secondary bonds is found to be approximately fifty. Thus, the primary bonds, or intramolecular forces, are about fifty times as strong as the secondary bonds, or intermolecular forces, for polyethylene single crystals. 3. For second nearest-neighbor interactions, thirty interaction constants have been found for polyethylene single crystals, as compared to only five such constants for crystals having simple cubic symmetry. For first neighbor interactions only, these constants become eleven in number, as against two for cubic crystals. On application of a limited central force assumption to the forces between units belonging to different chains, the numbers of constants for second nearest- 76 77 neighbors have been reduced to fourteen for polyethylene single crystals and two for cubic crystals. In the latter case, however, no limitation is imposed on the central force assumption. The corresponding numbers for the first neighbors become seven and one. 4. Interaction constants for units belonging to the same chain turn out to be 103 -105 times higher in value than those for units belonging to different chains, the former being of the order of 1-3 x 10..3 dyne/A, whereas the latter have a magnitude ranging from 3 x10“6 to 9 x10.8 dyne/A. 5. Interaction constants for units having a separation distance less than 4. 493 A are positive, while, for others having higher separation distances they are negative. The magnitudes of the positive constants are found to be approximately 300 times the magnitudes of the negative constants for separations up to the most distant second neighbor. For higher order neighbors this factor will be still higher; but the true values of the elastic constants are approached very rapidly. In fact, second nearest neighbor inter- actions give values of the constants which are quite close to their acutal values. 6. The value of the elastic constant c is found to be about 33 200-1000 times the values of the constants C11 and C22' These constants are measures of the Young's moduli along their respective axes. The exact value of the former is C33 = 2. 42266 5 x10”4 dyne/AZ 78 which yields a value of Young's modulus of E3 = 2. 388100 x 10-4 dyne/Az that agrees with the observed value of Young's modulus for 4 dyne/A2 and is lower than the oriented polyethylene of 2. 6 x 10- value of 3. 4 x 10.4 dyne/AZ calculated by Shimanouchi (17). Values of the constants c11 and c22 are found to be: 6 dyne/A2 c 0.948127x10- 11 6 dyne/ A2 C22 0. 288779 x10 These yield values of the Young's moduli E1 and E2 as 0. 377123 x 10"6 dyne/A2 and 0. 266161 x 10-6 dyne/A‘Z and, thus, seem quite reasonable since the value of Young's modulus of bulk polyethylene is known to be about 10"5 dyne/AZ. This fall squarely between the minimum value 6 of 0. 266161 x 10' dyne/Az calculated for E2 and the maximum value of 2. 388100 x 10'4 dyne/AZ calculated for E3. _ 7. The constants C44, C55 and C66 have been calculated to be: -4 2 644 = 1.123761 x10 dyne/A -4 2 C55 _ 0.866595 x 10 dyne/A -7 2 C66 _ 6.515515 x 10 dyne/A Thus, polyethylene single crystals are found to have shear resistance even when only first nearest -neighbor interactions are considered and the central force assumption is applied. This is in direct contrast to cubic crystals, for which shear resistance is introduced by considering the second neighbor interactions. The shear moduli C44 and css, which involve movements of units belonging to the same 79 chain, are found to be about 100-200 times the shear modulus C66, which involves movements of units belonging to different chains. 81 Due to the lattice units being of unsymmetrical shape, the forces between them are not quite central. It would be of considerable interest to determine the effect of these forces on the elastic constants of polyethylene single crystals. The interaction constants in such a case may be evaluated by taking their geometry and location into account. Bulk polyethylene is made up of spherulites which consist of randomly-oriented lamellae of single crystals. A future study could be directed towards finding how the elastic properties of spherulites are related to those of single crystals. This information may in turn be related to the elastic properties of bulk polyethylene. Investigations identical to the present work could be extended to include polymers having lattice structures such as tetragonal, hexagonal, monoclinic, triclinic, and rhombohedral. A comparison of the inherent anisotropies of these materials due to their lattice structures would then be possible. In many crystalline polymers hydrogen bonding provides the intermolecular forces, which are much stronger than the London dispersion-type of van der Waals forces. An investigation of the influence of hydrogen bonding on the elastic properties and, hence, the anisotropy of such polymers would be of considerable interest. 81 Due to the lattice units being of unsymmetrical shape, the forces between them are not quite central. It would be of considerable interest to determine the effect of these forces on the elastic constants of polyethylene single crystals. The interaction constants in such a case may be evaluated by taking their geometry and location into account. Bulk polyethylene is made up of spherulites which consist of randomly-oriented lamellae of single crystals. A future study could be directed towards finding how the elastic properties of spherulites are related to those of single crystals. This information may in turn be related to the elastic properties of bulk polyethylene. Investigations identical to the present work could be extended to include polymers having lattice structures such as tetragonal, hexagonal, monoclinic, triclinic, and rhombohedral. A comparison of the inherent anisotropies of these materials due to their lattice structures would then be possible. In many crystalline polymers hydrogen bonding provides the intermolecular forces, which are much stronger than the London dispersion-type of van der Waals forces. An investigation of the influence of hydrogen bonding on the elastic pr0perties and, hence, the anisotropy of such polymers would be of considerable interest. APPENDIX I EVALUATION OF SERIES In order to determine the Lennard-Jones 6-12 potential constants A and B (Section 2. 2), it is required to evaluate the triple series so AS : 2, m2: n: _m [(Zel)2 + (me2)2 + (ne3)z] '8/2 I-l for s = 6 or 12, and where Am both even or both odd, but )4 0 and n = any integer. As defined earlier , _ _3; _ el - 2 — 3.705 A _ E _ e2 — 2 — 2. 470 A _ E ._. e3 — 2 2. 550 A Dividing and multiplying by ef, I-l may be written as _ e 2 e 2 —s/2 A =esz[22+mZ(—Z—) +n2(—:1)] , l-Z s 1 e e 1 1 Substituting e Z 2 2 _ 2.470 _ (131-) — (3.705) — 0.444 e 2 Z 3 2.555 _ (ET) " '3.'7"05') ‘ 0'4” in I-2, we get AS : e1"S 23 (22 + 0.444 m2 + 0.474 n'2)'-S/2 I-3 = efs A' a I-4 s 82 83 where - 2 A; = 2 (£2 +0.444 m2 +0.474 n2) S/ with the same conditions on 2, m, n as in I-l. This triple series of I-5 is separated into single, double and triple series to find its value. These component series are evaluated as follows: Si_ngl£ Series For m, n = 0, we have so 00 _ 2 2'S=2223=2a , 1-6 ‘:—CD [:2 S where °° -s a : E 2 for .8: even only 3 2:2 I-7 or '00 l 21/ _ Z) __ _ - aZU — n=1 (Zn for n — any integer and s=2v=even . Similarly for 2, n = 0, we have °° 2)-s/2 gm (0.444 m 2 (0.444)'S/2 aS . 1-8 m An exact method of finding the value of this single series is given by Knopp (29), by which 00 21/ l _ V-l 1211'? 1:1 nzu ‘”'") 2.(2v): Bzu ' 1’9 where n is any integer, and B's are Bernoullian numbers. The first few of these numbers are _ _1 _1 _ 1 __1_ _ 691 36‘1'31‘2'32‘6'34‘ ”30' B6‘42' 1312 '2730 ° 1-10 and B3=B5= °=B2V+1:O for 2V+l:3. Expression I-9 for odd terms only is °° 1 v-l Q6)“ -11'2V 2 _fi = (‘1) 2 (2u)' 1'11 n=1 (Zn-l) ' ' This is obtained from I-9 by substracting the series for even terms 12 2v _ 0° 1/ _ V -1 1r as — Z (2;) — (-1) m B21! I-lZ n=1 Setting 3 = 21/ = 6 in I-12 yields: a - 3% l -( 1)2 "6 B I 13 _ _ - t - 6 n=1 (2n)6 2.(6). 6 Substituting 36 = 217 from 1-10 in 1-13, we get a6 = 0. 015895916 . I-14 Similarly for s = 12, we have: m 12 l 5 11' a = Z —-— = (-1) —""'— B 1'15 12 n=1 (2n)12 2.(12)1 12 . . _ 691 . Substituting B12 — - _2730 from I-10 in I-15, we get a = 0.000244198 . I-16 12 85 Double Series For n = 0, we have so 2 2 -s/Z E (2 + 0.444 m ) e I, m: -°° cn 2 Z -s/2 4 2(1 +0.444m) = 4bs. 1-17 I, m=2 where 00 -s/2 b = 23 (£2 + 0. 444 mg) for l, m = even only. S I, m=2 I-18 Similarly for m = 0, we have °° 2 2 '5/2 >3 (2 +0.474n) :4b' , 1-19 2, n: -°° s where °° 2 2 .8/2 for t = even only and b' = z (2 +0.474n) S 2:2, n=1 n 2 any integer; I-20 and for l = 0, we have °° 2 2 '5/2 E (0.444m +0.474n) 24b", I-21 m, n: -°° S where co 2 2 -s/Z b" = 2 (0.44m +0.474n) s m=2,n=l for m = even and n = any integer. I-22 86 The double series bs’ b's and by are evaluated by direct summation, and to do this with reasonable accuracy all the terms whose c ontributi on is 3 1 < — z = (40) 0.000015 for s 6, and is 1 6 < '46) z 0.00000000024 for s :12, are neglected. Such a termination of these sums is justifiable because of the fast convergence of the series. Though the number of terms increases rapidly with the increasing values of l, m and n, the order of error involved would still be small because, first, the size of the polyethylene crystals is small (being finite) and, secondly, the contribution of only the first few terms is significant as compared to higher order terms. Thus: b6 = 0. 34911017055 0‘ ll 0.101079817615962 12 b'6 = 0.01782841530 1-23 bl2 2 0.0001156995141015 b" = 0.1201500514 b'l'Z = 0. 008143632999903 Trixie Series We have as -s/Z 2 (£2 + o. 444 m2 + o. 474 n2) to ma 1'1: -0) 8c , I-24 where Evaluating the sums cS double series, we have: (1‘2 + 0. 444 m 87 2 -s/2 2+0.474n) for i, m even and 11 any integer. I-25 with the same order of accuracy as for C6 = 0.20449870704 I-Z6 clz = 0.0209123979253897 Rewriting the A'S of I-5 as; - 2 °° 2 2 2 S/ I _ AS _ ,m,n:_m(2 + 0.444m +0.474n) 00 ‘30 -s/Z = 2 z: 2'5 + 2 2 (0.444m2) 2:2 m=2 co 2 Z -s/Z co 2 2 -S/Z +4 23 (2 +0.444m) +4 2 (2 +0.474n) f, m=2 .12, 11:1 °° 2 2 ‘8/2 +4 2: (0.444m +0.474n) m=2,n=l °° 2 2 2 '3/2 +8 2 (2 +0.444m +0.474n) . 1-27 ,m=2,n=1 we have -s/2 A'=2(l+0.444 )a +4(b +b'+b")+8c . S S S S S S I-28 Substituting 0.444“3 = 0.087528384 for s— 6 88 and 6 0.444" = 0.0076612 for 5 =12 in I-28, we have A' = 2.175056768a 6 +4(b6+b' 6+bé‘)+8c6 6 and ._ I A' - 2.0153224a +4(b12+b +b'1'2)+8c 12 12’ I-29 12 while substituting the numerical values of as, bs’ b's, b's' , cS in the above, yields: Aé = 3. 97935343732 1-30 '12 = 0. 6673191079229836 To obtain numerical values of the sums AS , these numerical values of A; must be substituted. Thus, for s = 12 and 6 -12 A12 2 61 A12 and 1-31 ._ '6 1 A6 — 61 A6 3 where e1 = 3.705A such that el'l‘2 = 2, 587.95131"Z 14'12 and I-32 e'6 = 2, 587.95131'1 A'6, 89 Substituting I-32 in I-31, gives A12 = 9.96372 x10.8 14'” and I-33 A6 = 1.537646x10“3 A’6 Now, from 2. 43 , A12.6 : I"”‘12 'A6 ' where p =-:- (r0)6 =—:— (4. 45)6 =% (7, 795.23947455) = 3, 897.6197 A6 ; 1-34 therefore, __ -3 -6 A _ -l.149298x10 A . 1-35 12-6 APPENDIX II TRANSFORMATION OF PARTIAL DERIVATIVES Let ci. be the direction cosines of the axes x', y', z', with reapect to the axes x, y, z, as illustrated in the figure given bdow showing only the x' axis. Figure II-l. Rotation of axes. Thus, C11:C°S 0., c12=cos (3, c13=cosy II-l such that ._. l l I x—cllx +c21y _+c3lz y = ch x' + c22 y' + C32 2' II-Z _ i I l z—cI3x +c23y +c33z Differentiating II-2 with respect to x, y, 2, respectively, yields 3x _ 8 _ 32 _ . a? " C11' . 35 “ °21’ ’63? " C31 ° H'3 90 91 If a displacement function q is given as q = q(x, y, z) II-4 then 231 z 23 2:; 23 :31 9.4 23 - and ex the + By 3x' + 8x the ° H 5 Substituting from II-3 into II-5 results in 9.9. = 9.9. 23 29. - - the C11 3x “:21 8y +C31 az ' H 6 and differentiating II-6 again, we get 2 2 2 2 a 9 = _8__ 5’51 8 a. 3 a ,2 3x' (3):") ' c11 “11 + C21 axay " C31 3x3z) 3x 3x 2 2 2 a a a + C21 “11 8x3 + C21 3y l c31 ayaz) 829 829 82 + c31 (C11 axaz + c21 ayaz + ('31 32%) 2 2 2 2 _ 2 a g 2 a 2 a g a 9 " c11 2 +821 ‘2' + c31 2 +2C11°218x8y 3x By 32 2 2 . . 3 L9. +2 °11¢31 xaz + 2 °21°31 ayaz ' II-7 It is required to transform second partial derivatives of the displacements with respect to the axes x12, x21; x13, x31; x23, x32; x1 ,3, 1:31,; x1,,3, x31“ into partial derivatives with respect to x, y, 2. In order to do so, the direction cosines of these axes are needed. They are listed below along with the corresponding axes. x31' x1"3 x3111 ( a . -—P-— . 0 ) Va2+b2 .1542 ( ' a 9 b i 0 ) Vaz+bz «I 2+bZ ( a . o . C ) N/a2+c N/az +cz ( ' a a 0 9 C ) Va2+cz N/a ( o . b . ° ) N/bz+c2 Vbz Z ( O , _ b c ) N/bz+c2 «I b ( a b c ) Va2+bz+4c2 Klaz +b 2+4c2 Va2+bz+4cz ( _ a. _ b C ) N/a2+b2 +4c2 Vaz+bz +4cZ N/a2+b2 +4c2 (- a b 2C ) Va2+b2+4c2 Vaz+bz+4cz ~la2 +b z+4eZ ( a. - b 2C ) v 2 Z 2 ’ ’ a “D +4° ~laz+bz +4e2 Va2+b2+4c2 II-8 93 Thus, for differentiation with respect to the x12 axis, we have .33 -23-_2_§_i+_‘2__251 3x - ax' '- 12 N/az+bz Vaz+bz and differentiating again 2 9.9..=_L(§_9_)._.__a__(_2__9_3+____ 8x2 ax' 3’“ 2 2 2 2 8x2 12 «la +b N/a +b b a all + (~— 2 2 2 2 3"" N/a +b N/a +b 01' 2 2 32 2 —§-3 = a2 —‘216 +Zab-g—9— + b2 __g_6 2 ) 3x12 a 2+b 8x 8y Similarly for the ax1s x21 2 2 2 2 a _ 1 2 a a 2 a +_ 22 (a—§-2abaa+b —29-) £3le a +b 3x 3y Adding II 9 and II 10 yields 029 + 629 _ 1 2 82 +21)2 82 ) 2 " 2 2 6x12 8x21 a +b 3x By and subtracting II-lO from II-9 gives 2 2 89 _ 3 _ 4 ab 6 2 2c _ 2 2 5x5‘y ' 3x12 8x21 a +b Repeating the above operation for the other sets, we have 2 Z Z Z 3 3 g 2 3 Z 3 9 3x 3x a 2+b 3x 82 8x 3y b 32 2 2 5‘33’) Va +b b 829 ) 2 a 7‘ a +b y 11-9 . 11-10 , 11-11 11-12 11-13 94 8 8 _ 4ac 8 _ f2" ' “—13 2 - 7:2 82 ' ”'4 x13 x31 3 2 2 2 2 - 2 §_§_+§_g_=-%——2(2b923 ,+2c a ), 11-15 8x23 8x32 b +c " ' 8y 82 2 2 2 1%.. .. 9.1L = .2422. _3_9_ ; II-16 8 8 2 b +2 8y82 "23 x32 C 2 2 2 2 2 8x13 8x31, +b +4e 8x Y 8y 2 32 + 8 —9-2 ), 1117 82 82 32 1 82 82 firm—im (8a°8719“+8b°8'%’)' 11"" a a +b +4 x z Y z Xl,3 X31, a C 2 2 2 2 2 a +——9—a =———————2 12 2(2a2__382 -8ab-g;%—+2bza 8x1”3 8x231” a +b +4c 8x y 8y 2 +8cz a—-g-) , II-l9 82 829 829 132 a2 " 2 zTT‘T"8a°8xaz ”“8“???" “'20 1:1,,3 8x31” a +b +4c 2 a2 a2 1 2 a2 3% +_2q_ + _.9._ +§_9_ = (4a a a a 2 a 2+b2+4 Z a x1'3 x31' x1H3 x31H a C Y 2 2 +4bZ9—% +1667“? ). 8y 82 11-21 2 2 2 2 2 ’ a _89 + 39 ___9._3 =——————' (16bc——‘1-a ). 2 2 2 2 2 2 8y8z 8x1,3 8x31, 8x1”3 8x31” a +b +4c II-22 - 1 . .‘...u_\?-"' 95 Equations II-9 through II-22 are the transformation. relations utilized in deriving the expressions 2.63 -65 from 2.60-62- _‘ .-. r1'.n:5.." b . I] 7.. APPENDIX III STRAIN ENERGY CONNECTION BETWEEN THE ELASTIC AND INTERACTION CONSTANTS In Section 2. 3, the elastic constants were obtained in terms of the interaction constants from a comparison of the equations of motion derived from continuum and disc ontinuum theories. Second nearest-neighbor interactions were considered; and the expressions ! thus obtained were simplified for first nearest-neighbors only and a , limited type of central force assumption. Expressions identical to } these (2. 78) may also be obtained from strain energy considerations. In this appendix an expression for the strain energy is derived by considering motions of the first nearest-neighbor lattice units relative to the central unit. This is then compared with the corresponding continuum Expressions 2. 22: of the Section 2.1. First nearest-neighbors surrounding a central unit (0, 0, 0) are shown in Figure 2. 5 in Section 2. 3. Using the same notations as were used for the secondnearest-neighbors, the strain energy per lattice unit uI in terms of displacements u, v, w and the interaction constants, under the central force assumption becomes: u = -'—k '1 (u -u )2 +3.1. (v 1" I 2 k100 100 000 2' 0k10 "010 “000 1 k11 1 k33 +‘2'k001(“001'“000) +2'k001'"001"’000' +2 k001‘w001'w000) +-1-1<1 [(u1 )2 + (u -u ) ] 2 k1100 1100 u000 11100 000 1 k22 2 "2" 1.100 [("1100""000)Z + ("11100'"000' ] 111-1 96 97 By dividing each term of the above expression by the appropriate lattice distance and using the well known finite difference relations we obtain: 1 2 k11 u2 1 2 k22 1 2 “1:2" k100(8x) "'2'" "010‘8YZ' *2 ° ["001('5?) k22 “L" 001 (az'z + "001 (T) 2] a+z 8v 2 + ___:{k1100[('g:l_' )2+(ax212) ] +k1|zoo[(Taav 2)2+(‘5;;) ]} III-2 Once again,by transforming differentiations with respect to x12 and x21 into those with respect to x, y, 2, III -2 may be written as: “1:2'a2"l00'ax'z"b2"121l0'a;2) +“210(111'522) + k001(82 v2) +"001(6):; ”)2” +-l-{kl [a —-:—+b + b 8“2] 8 "1100("%’ 8')2 “it" y) . 2 ”(lizoo[(a%—b%1)2+(a%§'b%yi)]} III-3 which may rewritten by collecting coefficients of the respective partial derivatives as: ___ k11 1k 2 11 (:2 k11 “13‘2"100+4"1100"ax‘y) +71?" "1100 (a) "'2' "001%?2 1 2 22 k22 1 1 c2 k22 +4" "1100('5;t')Z “’2 (2' "010"? 1100) (15"'2c "8001(2‘3' 1 2 k33 + 2 C "001 "67’2111'4 98 To obtain an expression for the strain energy density, let us multiply both sides of the above by the number of units per cell and divide by the volume of the unit cell. From Figure 2. 2, we have 8013-) + 2 Q) = 2 111—5 number of lattice units per cell volume of the unit cell = abc . Thus, the strain energy density U in terms of uI may be written as: 2 uI abc HI - 6 U : The corresponding expression from continuum theory is: _ 1 2 r 2 2 U ‘ '2' (“1151 + c22'52 + c3363) + (“126162 + c13‘51'53 + °23€2‘3) 2 1 2 2 + '2' (C4464 + C5565 + c6666) which, on substitution for the values of Ej from 2. 5 and 6, yields: _ 1 8u 2 8v 2 8w 7- U - 2[°11 (8;) 1“sz5:," ”3318;” +[c12 ($1 63%) + cl3 (3%) (133) + c23 (3%) ($21)] 8u2 2 l 8v 8w 8w 8v 8u2 ”'2' °44'8‘2 "8;" + c55 Wilt)?" + C66 ('5;+§7) ] 111--7 Collecting coefficients, this may be rewritten as: l 1 Bu 2 1 U = “___ 8u2 8u2 1 av?- 2' C1195) +2°66 "2°55'52') +2°66"5§' l 8 l 8v)2 2 2 v +2"sz ('83?) *2 C44 (“8" 1 8w 2 1 8w 2 1 8w 2 "2655(7)? +2°441871 +2°33 (8'2" 213 '21 9.13 2111.. 9.1.1 211.11 + c12 (8x) (By) J” C13 (axl (82) + <323 (8y) (82) 8v 8w 8w 8u 8v 8u 99 Comparing III-4 and III-8 by using III-6, we obtain the following 11 expressions for c.. in terms of k! 13 mm 11 ll 611 = 15% ("100 +'i’"1100' C22 '"‘ 2": ("0:0 + 2":1200) C33 = {CH- "001 a (:44 = 2913 "301 °r “44 = 0 c55 = 3215 "(1101 °r (‘55 = 0 C 1.21.11 ._.1. 66 ' 2 ac 1'00" 2 bc 1'00 C12 = 0 ‘213 -= 0 C23 = 0 0 111-9 Except for C12’ C13 and c23 these are identical to the Expression 2.78. Even redundancy in expressions for C44, c55 and C66 is same as before. This provides a check on the two procedures. Such an agreement will not, however, be obtained if non-central forces are considered because different higher order terms are neglected and included in the two cases. APPENDIX IV A NOTE ON THE LENNAR Dl-JONES POTENTIAL Intermolecular forces are approximated by a 6-12 Lennard- Jones potential, (Mr) = l2 - —%— 2.26 1‘ 1‘ 01' 1' . r . ¢(r) = e[:2( Tm)” wig—13f] . 1v-1 Both of these forms are listed by Hirschfelder, et a1 (21). The first is used herein, and this is also the form employed by Born and Huang (23). However, 'Peterlin, et a1 (30), McMahon and McCllOugh‘Gl) use variations of the second. Further, they employ one potential along the b-axis and another along the diagonal (a, b) axis, thus calculating different values of rmin along these directions. This is probably done because of the inherent properties of the orthorhombic lattice of poly- ethylene: (i) There is an additional unit at the midpoint of the rectangle (a, b). (ii) This unit is at a distance of -lz--1\/a2 + b2 , which is not equal to b. (iii) The unit has an orientation different from the corner units. Nevertheless, a closer study of the lattice structure of poly- ethylene reveals that such difficulties may be resolved without using different potential forms in different directions. 100 101 b a A / / \ //r4=2.63A ‘\ ' / \rl / \ l // b\\ x / r3 =./2.£3 r' \ \\\ \ / [I \\ 171:2.63 \\~ / \\ \ ___- —r' - \ ._. - \. \ r 2 63A H \\2— ° 1'3 \‘ '\ l \\ \ V Figure IV-l. Detailed positions of the hydrogen atoms in the (a, b) plane. 102 Figure IV-l is a detailed drawing of a single cell of polyethylene in the plane (a,b), showing the positions of the hydrogen atoms in space relative to each other. It may be observed from this figure that the separation distances r1, r2, r3 and r4 of the hydrogen atoms are all equal. This suggests that: (i) The geometry of the polyethylene molecules and their location in space determine the lattice structure. (ii) The London dispersion forces between hydrogen atoms determine the Lennard-J ones potential such that the hydrogen atoms are at equilibrium separation. Thus, the net force between any two lattice units in a plane is a result of the interaction of their hydrogen atoms. The potential between the two nearest hydrogen atoms can be written as ¢'(r) = if? - 1' IV-2 "04"? where the ratio of A' and B' is determined by their equilibrium distance r2) . The net potential 4) between the two units at the lattice points is: 49(1') = 2[¢'(r1)+ ¢'(r2)+ 9'.(-r3) + ¢'(r4)l + 2 [ ¢'(ri) + ¢'(r'2) + 1l>'(r'3) + 11>'(1r11)] = 8 [ 4111-10) + ¢1(r1)] Iv-3 10. ll. 12. 13. 14. 15. ’ VI. BIBLIOGRAPHY P. H. Lindenmeyer, J. Polymer Sci. 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