Optimal design of laminated composite shells-Reference-Cited by-同舟云学术

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Optimal design of laminated composite shells

Published:1981-04-06 Issue: Volume: Page:
ISSN:
Container-title:22nd Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

NSHANIAN Y.¹,PAPPAS M.²

Affiliation:

1. Armianskii Sel'skokhoziaistvennyi Institut, Yerevan, Armenian SSR

2. New Jersey Institute of Technology, Newark, N.J.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1981-555

Reference13 articles.

1. Optimum Design of Laminated Plates under Axial Compression

2. Nshanian, Y.S. , and Pappas, M."optimal Design of Laminated Composite Plates", NJIT Report NV-16, April 1981. 5, Bushnell,D."Buckling of Shells-Pitfalls for Designers", Proceedings of the 21st Structures, Structural Materials and Dynamics Conference, Held a t Seattle, Wash., May 12-14, 1980, Part I, pp.1-56.

3. Instability of composite panels

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Optimum design of composite laminates with STROPT;Communications in Numerical Methods in Engineering;1993-11

2. Optimal laminated composite shells for buckling and vibration;AIAA Journal;1983-03

3. Optimal design of laminated composite shells;22nd Structures, Structural Dynamics and Materials Conference;1981-04-06

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