Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels-Reference-Cited by-同舟云学术

Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels

Published:1996-01 Issue:5 Volume:27 Page:519-526
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Jaunky Navin,Knight Norman F.,Ambur Damodar R.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference14 articles.

1. Damage Tolerance of a Geodesically Stiffened Advanced Composite Structural Concept for Aircraft Structural Applications;Rouse,1991

2. Effect of Stiffness Characteristics on the Response of Composite Grid-stiffened Structures;Ambur;AIAA Paper No. AIAA-91-1087-CP,1991

3. Buckling Results of Stiffened Panels Subjected to Combined Longitudinal Compression and Shear: Results Obtained with PASCO, EAL and STAGS Computer Programs;Stroud;NASA TP 2215,1984

4. Optimal Design of Geodesically Stiffened Composite Cylindrical Shell;Gendron;AIAA Paper No. 92-2306-CP,1992

5. Discrete analysis of stiffened composite cylindrical shells;Wang;AIAA J.,1985

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