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Table 2
Experimental and numerical identified Hill's 1948 coefficients of AA2024-T351 thick plate [9–11].
Hill parameters (MPa) | F | G | H | L = M = N |
---|---|---|---|---|
Experimental plane anisotropy ( = 12%) | 0.64 | 0.62 | 0.38 | 1.74 |
Experimental normal anisotropy ( = 12%) | 0.60 | 0.60 | 0.40 | 1.40 |
Numerical identification of plane anisotropy | 0.50 | 0.63 | 0.37 | 0.97 |
Numerical identification of normal anisotropy | 0.63 | 0.63 | 0.36 | 1.35 |
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