The design, testing and analysis of aeroelastically tailored transonic flutter model wings-Reference-Cited by-同舟云学术

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The design, testing and analysis of aeroelastically tailored transonic flutter model wings

Published:1983-05-02 Issue: Volume: Page:
ISSN:
Container-title:24th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

MURPHY A.¹,ROGERS W.¹,SHIRK M.²,RUHLIN C.³

Affiliation:

1. General Dynamics Corp., Fort Worth, TX

2. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OH

3. NASA, Langley Research Center, Loads and Aeroelasticity Div., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1027

Reference4 articles.

1. Rogers, W. A., Braymen, W. W., Murphy, A. C., Graham, D.H., and Love, M. H. Validation of Aeroelastic Tailoring by Static Aeroelastic and Flutter Tests, AFWALTR-81-3160, A i r Force Wright Aeronautical Laboratories, Wright-Patterson A i r Force Base, Ohio

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. Experimental Aeroelasticity - History, Status and Future in Brief;31st Structures, Structural Dynamics and Materials Conference;1990-04-02

2. Evaluation of four subcritical response methods for on-line prediction of flutter onset in wind tunnel tests;Journal of Aircraft;1983-10

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