I have carried out numerical first-principles calculations of the pressure dependence of the elastic moduli for several ordered structures in the aluminum-lithium system, specifically fcc Al, fcc and bcc Li, L1₂{Al}₃$Li, and an ordered fcc ${Al}₇$Li supercell. The calculations were performed using the full-potential linear augmented plane-wave method (LAPW) to calculate the total energy as a function of strain, after which the data were fit to a polynomial function of the strain to determine the modulus. A procedure for estimating the errors in this process is also given. The predicted equilibrium lattice parameters are slightly smaller than found experimentally, consistent with other local-density-approximation (LDA) calculations. The computed elastic moduli are within approximately 10% of the experimentally measured moduli, provided the calculations are carried out at the experimental lattice constant. The LDA equilibrium shear modulus C₁₁-C₁₂ increases from 59.3 GPa in Al, to 76.0 GPa in Al₇Li, to 106.2 GPa in Al₃Li. The modulus C₄₄ increases from 38.4 GPa in Al to 46.1 GPa in Al₇Li, then falls to 40.7 GPa in Al₃Li. All of the calculated elastic moduli increase with pressure with the exception of bcc Li, which becomes elastically unstable at about 2 GPa, where C₁₁-C₁₂ vanishes.
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Michael J. Mehl (1993) studied this question.
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