Influence of warpage on composite aeroelastic theories-Reference-Cited by-同舟云学术

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Influence of warpage on composite aeroelastic theories

Published:1985-04-15 Issue: Volume: Page:
ISSN:
Container-title:26th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

OYIBO G.¹,BERMAN J.¹

Affiliation:

1. Fairchild Republic Co., Farmindale, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-710

Reference19 articles.

1. 8: + 16 = B: ( B 2- 2 16 h c) 2 = 8' 1

2. t B I B z sin B1 -8,B; sinh B2),

3. Not i c e

4. Frequency Parameter versus l/(So/co

Cited by 7 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. Bounds on Flexural Properties and Buckling Response for Symmetrically Laminated Composite Plates;Journal of Engineering Mechanics;2007-11

2. Exact solutions to the oscillations of composite aircraft wings withwarping constraint and elastic coupling;AIAA Journal;1990-06

3. Formulation and Evaluation of An Analytical Model for Composite Box-Beams;31st Structures, Structural Dynamics and Materials Conference;1990-04-02

4. Some implications of warping restraint on the behavior of composite anisotropic beams;Journal of Aircraft;1989-02

5. Supersonic flutter of aeroelastically tailored oblique wings;Journal of Aircraft;1989-01

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