Optimization of an Axially Compressed Ring and Stringer Stiffened Cylindrical Shell with a General Buckling Modal Imperfection-Reference-Cited by-同舟云学术

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Optimization of an Axially Compressed Ring and Stringer Stiffened Cylindrical Shell with a General Buckling Modal Imperfection

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Bushnell David¹

Affiliation:

1. AIAA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2216

Reference107 articles.

1. PANDA2—Program for minimum weight design of stiffened, composite, locally buckled panels

2. A PRELIMINARY DESIGN PROCEDURE FOR COMPOSITE PANELS WITH OPEN-SECTION STIFFENERS LOADED IN THE POST-BUCKLING RANGE

3. General Panel Sizing Computer Code and Its Application to Composite Structural Panels

Cited by 2 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. An Experiential Optimization Design Method for Orthogonal Rib-Stiffened Thin Walled Cylindrical Shells under Axial Loading;Applied Mechanics and Materials;2011-10-24

2. Use of GENOPT and BIGBOSOR4 to obtain optimum designs of an axially compressed cylindrical shell with a composite truss-core sandwich wall;52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2011-04-04

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