Recent Developments in the Design, Testing and Impact-Damage Tolerance of Stiffened Composite Panels-Reference-Cited by-同舟云学术

Recent Developments in the Design, Testing and Impact-Damage Tolerance of Stiffened Composite Panels

Published:1980 Issue: Volume: Page:259-291
ISSN:
Container-title:Fibrous Composites in Structural Design
language:
Short-container-title:

Author:

Williams Jerry G.,Anderson Melvin S.,Rhodes Marvin D.,Starnes James H.,Stroud W. Jefferson

Publisher

Springer US

Link

http://link.springer.com/content/pdf/10.1007/978-1-4684-1033-4_15

Reference14 articles.

1. Mikulas, Martin M., Jr.; Bush, Harold G.; and Rhodes, Marvin D.: Current Langley Research Center Studies on Buckling and Low-Velocity Impact of Composites Panels. Third Conference on Fibrous Composites in Flight Vehicle Design, Part II, NASA TM X-3377, 1976, pp. 633–663.

2. Wittrick, W. H.; and Williams, F. W.: Buckling and Vibration of Anisotropic or Isotropic Plate Assemblies Under Combined Loadings. Int. J. Mech. Sci., Vol. 16, 1974, pp. 209–239.

3. Almroth, B. O.; and Brogan, F. A.: The STAGS Computer Code. NASA CR-2950, February 1978.

4. Williams, Jerry G.; and Stein, Manuel: Buckling Behavior and Structural Efficiency of Open-Section Stiffened Composite Compression Panels. AIAA J., Vol. 14, No. 11, Nov. 1976, pp. 1618–1626.

5. Stein, Manuel; and Williams, Jerry G.: Buckling and Structural Efficiency of Sandwich-Blade Stiffened Composite Compression Panels. NASA TP 1269, September 1978.

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