A benchmark elasticity solution for an axisymmetrically loaded angle-ply cylindrical shell

Composites Engineering - Tập 3 - Trang 1065-1073 - 1993
K. Bhaskar1, T.K. Varadan1
1Department of Aerospace Engineering, Indian Institute of Technology, Madras 600 036, India

Tài liệu tham khảo

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