Design of Practical Composite Structure Using Enhancements to MSC.Nastran Structural Analysis and Optimization-Reference-Cited by-同舟云学术

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Design of Practical Composite Structure Using Enhancements to MSC.Nastran Structural Analysis and Optimization

Published:2002-04-22 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Barker Daniel¹,Johnson John¹,Johnson Erwin²,Layfield Dale²

Affiliation:

1. Lockheed Martin Aeronautics Company

2. MSC.Software Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1339

Reference17 articles.

1. An ASTROS application with path dependent results

2. Optimum wing shape for an active flexible wing

3. AEROELASTIC TAILORING OF COMPOSITE MATERIALS TO IMPROVE PERFORMANCE

4. Eisenmann, J.R. "Advanced Composite Panel Optimization," General Dynamics Convair Aerospace Division for Wright-Patterson Air Force MaterialsLaboratory, FZM-6118, April 2,1973.

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. Impact of Actuation Concepts on Morphing Aircraft Structures;45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;2004-04-19

2. Optimization Strategies for the F/A-22 Horizontal Stabilator;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07

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