Flutter of forward swept wings, analyses and tests
Author:
Affiliation:
1. Purdue University, West Lafayette, IN
2. USAF, Wright Aeronautical Laboratories,Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-646
Reference19 articles.
Cited by 16 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. Aeroelasticity Research at Wright-Patterson Air Force Base (Wright Field) from 1953-1993;Journal of Aircraft;2003-09
2. Aeroelastic Tailoring of Joined-Wing Configurations;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22
3. Aeroservoelastic tailoring for gust response of a typical section aeroelastic model;36th Structures, Structural Dynamics and Materials Conference;1995-04-10
4. Structural Modeling of Low-Aspect Ratio Composite Wings;34th Structures, Structural Dynamics and Materials Conference;1993-04-19
5. Parametric aeroelastic stability analysis of a generic X-wing aircraft;Journal of Aircraft;1990-07
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