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Volume 6, Article 3
Robert R. Reeber, Kai Wang
Department of Materials Science and Engineering, North Carolina State University
A material at absolute zero is uniquely represented by the nature of its atoms, their spatial arrangement and the forces between them. In the rigid ion model it is assumed that the electron distribution is locked to the nuclei and is not affected by the lattice dynamics induced by increases in temperature and pressure. As one explores the state of matter at higher temperatures and pressures it is anticipated that most models will have increasing inaccuracies as interatomic interactions responsible for materials behavior are complex, generally non-linear, and are not well understood. Shell representations provide qualitative results for this difficult problem. First principle theories for calculating high temperature elastic constants have many approximations and assumptions and, as indicated earlier [3] [4], have difficulty in reproducing thermal expansion measurements over extended temperature ranges. Calculations of high temperature elastic constants [5] based upon the central force model of Keating [6] [7] also have been questioned on theoretical grounds [8]. Most of the theoretical work provides zero K results for the temperature dependence of assumed quasi-harmonic cubic semiconductors.
It is well known that the thermophysical properties of crystal-chemically similar materials often can be simply correlated by corresponding states relationships [9]. The symmetry of such materials provides a specific mathematical framework for describing the distribution of the fully excited 3N frequencies of a mole of atoms or molecules of a specific crystal structure. The stronger the material the higher is the temperature range that equivalent vibrational modes become excited. Simple correlations for melting, phase transitions and brittle to ductile transition temperatures have been made earlier [10] [11] [12].
In this work we use Debye temperatures as empirical corresponding states parameters to determine the elastic constants of SiC, AlN, GaN and InN from measured elastic constants of CdS [13]. It is assumed that:
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Where:
for compounds A and B. Li and Bradt [14] have predicted the high temperature elastic constants for 6H α-silicon carbide. Their results are utilized as a test for our predictions.
Table 1 lists the experimental literature values of the elastic constants for SiC, GaN, AlN and InN at room temperature. Elastic constants of SiC as measured by several authors [15] [16] [17] are also given in Table 1. Table 2 provides our predictions for 6H-SiC. With the exception of a 13% difference for C13 the relative differences are significantly less than 7% with respect to Li and Bradt's [14] results. The calculated Young's modulus utilizing the Voigt-Ruess-Hill (VRH) average is within -2.3% at room temperature to +0.27% at 1250oK of Li and Bradt's results. Tables 3 , 4 and 5 provide our predictions for AlN, GaN and InN. The room temperature elastic constant values necessary for our calculations are based upon literature results [18] [19] [20] [21] [22] [23] [24] [25] [26] [27] [28]. The Young's moduli calculated from McNeil et al.'s data [19] for AlN are shown in Figure 1 with existing experimental data [18] [19] [20] [29] [30] [31] [32] [33] [34] [35] [36]. For GaN, the room temperature elastic constants are based on the average of consistent measurements [20] [22] [24] [26] [27]. For InN, theoretical values from Wright [37] are applied in our calculation. Although experimental data exists for InN, GaN results generated by the same authors are not consistent with others [28]. The temperature dependence of the Young's moduli for other compounds investigated are provided in Figure 2.
A complete set of the elastic constants for important semiconducting nitrides has been calculated over an extended temperature range by utilizing an empirical corresponding state relationship. Values shown for the experimentally measured Young's moduli of AlN of Lubis et al. [30] and Ruh et al. [33] are in reasonable agreement with our calculations. They had some porosity in their polycrystalline samples. At higher temperatures one might expect a brittle to ductile transition to occur. This would cause a reduction in the measured Young's modulus. Unfortunately the mechanical property data available for comparison with our calculations is too limited to determine if such a transition occurs. In any case our results should be useful for estimating relative thermal residual stress variations under different growth conditions.
[1] K. Wang, R. R. Reeber, Mater. Res. Soc. Symp. Proc. 482, 863 (1998).
[2] R. R. Reeber, K. Wang, J. Mater. Res. 15, 40 (2000).
[3] R. R. Reeber, K. Wang, J. Electron. Mater. 25, 63 (1996).
[4] R. R. Reeber, K. Wang, Mater. Chem. Phys. 46, 259 (1996).
[5] A. I. Gubanov, S. Y. Davydov, Sov. Phys. Solid State 14, 372 (1972).
[6] P. N. Keating, Phys. Rev. 145, 637 (1966).
[7] P. N. Keating, Phys. Rev. 149, 674 (1966).
[8] J. W. Martin, J. Phys. C 8, 2869 (1975).
[9]M. Blackman,"The specific heat of solids", Hdb. Phys. Vol. VII/I, 325 (1955) (No journal name recognized.)
[10] R. R. Reeber, Phys. Stat. Sol. A 26, 253 (1974).
[11]R. R. Reeber, "An empirical method for correlating and predicting melting and solid-state phase transformations", in The physics and chemistry of minerals and rocks, edited by R. G. J. Strens (John Wiley, New York, 1976), p. 469 (No journal name recognized.)
[12]R. R. Reeber, "Corresponding state aspects of the brittle to ductile transition in diamond and sphalerite-structure solids", in Fracture Mechanics of Ceramics; Vol. 6., edited by R. C. Bradt, A. G. Evans, D. P. H. Hasselman, and F. F. Lange (Plenum, 1983), p. 545 (No journal name recognized.)
[13] D. Gerlich, J. Phys. Chem. Sol. 28, 2575 (1967).
[14] Z. Li, R. C. Bradt, Int. J. High Tech. Ceram. 4, 1 (1988).
[15] G. Arlt, G. R. Schodder, J. Acoust. Soc. of Am. 37, 384 (1965).
[16] K. Kamitani, M. Grimsditch, J. C. Nipko, C. -K. Loong, M. Okada, I. Kimura, J. Appl. Phys. 82, 3152 (1997).
[17] S. Karmann, R. Helbig, R. A. Stein, J. Appl. Phys. 66, 3922 (1989).
[18]K. Tsubouchi, K. Sugai, N. Mikoshiba, "AlN materials constants evaluation and SAW properties on AlN/Al2O3 and AlN/Si", in 1981 Ultrasonics Symposium Proceedings, 1981 (IEEE. NewYork), p. 375 (No journal name recognized.)
[19] LE McNeil, M Grimsditch, RH French, J. Am. Ceram. Soc. 76, 1132-1136 (1993).
[20] C. Deger, E. Born, H. Angerer, O. Ambacher, M. Stutzmann, J. Hornsteiner, E. Riha, G. Fischerauer, Appl. Phys. Lett. 72, 2400 (1998).
[21] V. A. Savastenko, A. U. Sheleg, Phys. Stat. Sol. A 48, K135 (1978).
[22] A. Polian , M. Grimsditch , I. Grzegory , J. Appl. Phys. 79, 3343-3344 (1996).
[23] Y. Takagi, M. Ahart, T. Azuhata, T. Sota, K. Suzuki, S. Nakamura, Physica B 219/220, 547 (1996).
[24] M. Yamaguchi, T. Yagi, T. Azuhata, T. Sota, K. Suzuki, S. Chichibu, S. Nakamura, J. Phys. C 9, 241 (1997).
[25] R. B. Schwarz, K. Khachaturyan, E. R. Weber, Appl. Phys. Lett. 70, 1122 (1997).
[26] T. Deguchi, D. Ichiryu, K. Toshikawa, K. Sekiguchi, T. Sota, R. Matsuo, T. Azuhata, T. Yagi, S. Chichibu, S. Nakamura, J. Appl. Phys. 86, 1860 (1999).
[27] M. Yamaguchi, T. Yagi, T. Sota, T. Deguchi, K. Shimada, S. Nakamura, J. Appl. Phys. 85, 8502 (1999).
[28] A. U. Sheleg, V. A. Savastenko, Inorg. Mat. 15, 1257 (1979).
[29] K. M. Taylor, C. Lenie, J. Electrochem. Soc. 107, 308 (1960).
[30] A. H. Lubis, N. L. Hecht, J. G. A. Graves, J. Am. Ceram. Soc. 82, 2481 (1999).
[31] D. Gerlich, S. L. Dole, G. A. Slack, J. Phys. Chem. Sol. 47, 437 (1986).
[32] P. Boch, J. C. Glandus, J. Jarrige, J. P. Lecompte, J. Mexmain, Ceram. Int. 8, 34 (1982).
[33] R. Ruh, A. Zangvil, J. Barlowe, Am. Ceram. Soc. Bull. 64, 1368 (1985).
[34] A. Kampfe, B. Eigenmann, O. Vöhringer, D. Löhe, High Temp. Material Processes 2, 309 (1998).
[35]G. Carlotti, D. Fioretto, L. Giovannini, L. Palmieri, G. Socino, L. Verdini, E. Verona, "1994 IEEE Ultrasonic Symposium Proceedings", in 1994 IEEE Ultrasonic Symposium Proceedings, 1994 (IEEE New York), p. 457 (No journal name recognized.)
[36]T. Shiosaki, T. Yamamoto, T. Oda, K. Harada, A. Kawabata, "Low temperature growth of piezoelectric AlN film for surface and bulk wave transducers by RF reactive planer magnetron sputtering", in 1980 IEEE Ultrasonic Symposium Proceedings, Boston, MA, 1980 (IEEE), p. 451 (No journal name recognized.)
[37] AF Wright, J. Appl. Phys. 82, 2833-2839 (1997).
Table 1
Room temperature elastic constants and Debye temperatures for SiC, AlN, GaN and InN.
| Compound | C11(GPa) | C12(GPa) | C13(GPa) | C33(GPa) | C44(GPa) | θD (K) | Ref. |
| GaN | 296.0 | 130.0 | 158.0 | 267.0 | 24.1 | [21] | |
| 390.0 | 145.0 | 106.0 | 398.0 | 105.0 | [22] | ||
| 374.0 | 106.0 | 70.0 | 379.0 | 101.0 | [23] | ||
| 365.0 | 135.0 | 114.0 | 381.0 | 109.0 | [24] | ||
| 377.0 | 160.0 | 114.0 | 209.0 | 81.4 | [25] | ||
| 370.0 | 145.0 | 110.0 | 390.0 | 90.0 | [20] | ||
| 373.0 | 141.0 | 80.4 | 387.0 | 93.6 | [26] | ||
| 373.0 | 141.0 | 80.0 | 387.0 | 94.0 | [27] | ||
| 374.2 | 141.4 | 98.1 | 388.6 | 98.3 | 637.3 | * | |
| AlN | 404.0 | [36] | |||||
| 345.0 | 125.0 | 120.0 | 395.0 | 118.0 | [18] | ||
| 410.5 | 148.5 | 98.9 | 388.5 | 124.6 | [19] | ||
| 102.0 | [35] | ||||||
| 410.0 | 140.0 | 100.0 | 390.0 | 120.0 | [20] | ||
| 424.0 | 122.0 | 166.0 | 353.0 | 123.0 | [34] | ||
| 410.5 | 148.5 | 98.9 | 388.5 | 124.6 | 965.2 | * | |
| InN | 190.0 | 104.0 | 121.0 | 182.0 | 9.9 | [28] | |
| 223.0 | 115.0 | 92.0 | 224.0 | 48.0 | 375.5 | * | |
| SiC | 500.0 | 92.0 | 564.0 | 168.0 | [15] | ||
| 504.0 | 98.0 | 566.0 | 170.0 | [15] | |||
| 564.9 | [17] | ||||||
| 501.0 | 111.0 | 52.0 | 553.0 | 163.0 | [16] | ||
| 479.3 | 98.1 | 55.8 | 521.6 | 148.3 | 1123.8 | * | |
| * Recommended values |
| T (K) | C11(GPa) | C33(GPa) | C12(GPa) | C13(GPa) | C44(GPa) | E(GPa) |
| 0 | 469.3 | 514.3 | 91.5 | 48.3 | 143.8 | 410.8 |
| 50 | 469.3 | 514.4 | 91.5 | 48.3 | 143.8 | 410.8 |
| 100 | 469.3 | 514.3 | 91.5 | 48.3 | 143.8 | 410.8 |
| 150 | 469.1 | 514.1 | 91.4 | 48.2 | 143.7 | 410.7 |
| 200 | 468.9 | 513.7 | 91.4 | 48.2 | 143.7 | 410.6 |
| 250 | 468.6 | 513.5 | 91.3 | 48.2 | 143.7 | 410.4 |
| 300 | 468.3 | 513.1 | 91.3 | 48.1 | 143.7 | 410.1 |
| 400 | 467.6 | 512.2 | 91.1 | 48.0 | 143.6 | 409.6 |
| 500 | 466.8 | 511.1 | 90.9 | 47.8 | 143.5 | 409.0 |
| 600 | 465.8 | 509.5 | 90.6 | 47.7 | 143.3 | 408.2 |
| 700 | 464.7 | 508.0 | 90.4 | 47.5 | 143.2 | 407.4 |
| 800 | 463.4 | 506.3 | 90.1 | 47.3 | 143.0 | 406.4 |
| 900 | 461.9 | 504.6 | 89.7 | 47.1 | 142.8 | 405.3 |
| 1000 | 460.4 | 502.9 | 89.4 | 46.9 | 142.6 | 404.2 |
| 1100 | 458.9 | 501.2 | 89.0 | 46.7 | 142.5 | 403.2 |
| 1200 | 457.2 | 499.6 | 88.6 | 46.5 | 142.3 | 402.1 |
| 1300 | 455.6 | 497.9 | 88.2 | 46.3 | 142.1 | 401.0 |
| 1400 | 454.1 | 496.2 | 87.9 | 46.1 | 141.9 | 399.9 |
| 1500 | 452.5 | 494.5 | 87.5 | 45.8 | 141.7 | 398.8 |
| 1550 | 451.8 | 493.6 | 87.3 | 45.7 | 141.7 | 398.3 |
| T (K) | C11(GPa) | C33(GPa) | C12(GPa) | C13(GPa) | C44(GPa) | E(GPa) |
| 0 | 411.6 | 385.5 | 148.9 | 99.4 | 124.1 | 329.2 |
| 50 | 411.6 | 385.6 | 148.9 | 99.4 | 124.1 | 329.2 |
| 100 | 411.5 | 385.5 | 148.9 | 99.3 | 124.1 | 329.2 |
| 150 | 411.3 | 385.2 | 148.8 | 99.3 | 124.1 | 329.0 |
| 200 | 411.1 | 385.0 | 148.7 | 99.2 | 124.1 | 328.9 |
| 250 | 410.7 | 384.7 | 148.6 | 99.0 | 124.0 | 328.7 |
| 300 | 410.5 | 384.3 | 148.4 | 98.9 | 124.0 | 328.5 |
| 400 | 409.7 | 383.4 | 148.1 | 98.5 | 123.9 | 328.0 |
| 500 | 408.7 | 382.1 | 147.6 | 98.1 | 123.7 | 327.4 |
| 600 | 407.5 | 380.8 | 147.1 | 97.7 | 123.6 | 326.6 |
| 700 | 406.2 | 379.4 | 146.6 | 97.2 | 123.4 | 325.8 |
| 800 | 404.7 | 377.9 | 145.9 | 96.7 | 123.2 | 324.8 |
| 900 | 403.1 | 376.4 | 145.2 | 96.2 | 123.0 | 323.9 |
| 1000 | 401.5 | 374.9 | 144.5 | 95.7 | 122.9 | 322.9 |
| 1100 | 399.9 | 373.4 | 143.8 | 95.3 | 122.7 | 321.9 |
| 1200 | 398.3 | 372.0 | 143.1 | 94.8 | 122.5 | 321.0 |
| 1300 | 396.7 | 370.5 | 142.4 | 94.3 | 122.3 | 320.0 |
| 1350 | 396.0 | 369.8 | 141.9 | 94.0 | 122.3 | 319.6 |
| T (K) | C11(GPa) | C33(GPa) | C12(GPa) | C13(GPa) | C44(GPa) | E(GPa) |
| 0 | 376.4 | 387.1 | 142.4 | 99.1 | 98.5 | 289.5 |
| 50 | 376.4 | 387.1 | 142.4 | 99.1 | 98.5 | 289.5 |
| 100 | 376.1 | 386.8 | 142.3 | 99.0 | 98.5 | 289.3 |
| 150 | 375.7 | 386.5 | 142.1 | 98.9 | 98.5 | 289.1 |
| 200 | 375.4 | 385.8 | 141.9 | 98.7 | 98.4 | 288.9 |
| 250 | 374.8 | 385.2 | 141.7 | 98.4 | 98.4 | 288.5 |
| 300 | 374.2 | 384.4 | 141.4 | 98.1 | 98.3 | 288.1 |
| 400 | 372.6 | 382.3 | 140.6 | 97.4 | 98.1 | 287.2 |
| 500 | 370.7 | 380.0 | 139.8 | 96.7 | 97.9 | 286.0 |
| 600 | 368.5 | 377.8 | 138.8 | 96.0 | 97.7 | 284.8 |
| 700 | 366.3 | 375.5 | 137.7 | 95.3 | 97.5 | 283.5 |
| 800 | 364.1 | 373.3 | 136.7 | 94.5 | 97.3 | 282.3 |
| 900 | 362.0 | 371.1 | 135.6 | 93.8 | 97.1 | 281.1 |
| T (K) | C11(GPa) | C33(GPa) | C12(GPa) | C13(GPa) | C44(GPa) | E(GPa) |
| 0 | 226.7 | 225.8 | 117.2 | 94.4 | 48.3 | 145.5 |
| 50 | 226.6 | 225.7 | 117.2 | 94.3 | 48.3 | 145.4 |
| 100 | 226.2 | 225.3 | 116.9 | 94.1 | 48.3 | 145.3 |
| 150 | 225.7 | 224.6 | 116.6 | 93.6 | 48.2 | 145.1 |
| 200 | 225.0 | 223.7 | 116.1 | 93.1 | 48.2 | 144.7 |
| 250 | 224.1 | 222.7 | 115.6 | 92.6 | 48.1 | 144.3 |
| 300 | 223.1 | 221.6 | 115.0 | 92.0 | 48.0 | 143.9 |
| 350 | 222.0 | 220.5 | 114.3 | 91.4 | 47.9 | 143.4 |
| 400 | 220.9 | 219.4 | 113.5 | 90.8 | 47.8 | 142.9 |
| 450 | 219.7 | 218.2 | 112.8 | 90.2 | 47.7 | 142.4 |
| 500 | 218.6 | 217.1 | 112.1 | 89.6 | 47.6 | 141.9 |
| Figure 1. Young's Modulus of AlN |
| Figure 2. Temperature dependence of Young's Modulus for AlN, GaN and InN. |
© 2001 The Materials Research Society
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