Multidisciplinary Design Optimization of a Built-Up Wing Structure with a Tip Missile-Reference-Cited by-同舟云学术

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Multidisciplinary Design Optimization of a Built-Up Wing Structure with a Tip Missile

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:

Jun Seungmoon¹,Tischler Victoria²,Venkayya Vipperla²

Affiliation:

1. Agency for Defense Development

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1421

Reference16 articles.

1. Effect of Store Aerodynamics on Wing/Store Flutter

2. Optimization of wing tip store modeling

3. Wind tunnel correlation study of aerodynamic modeling for F/A-18 wing-store tip-missile flutter

4. G. Guruswamy, P. Goorjian, and E. Tu, "Transonic Aeroelasticity of Wing with Tip Stores", AIAApaper 86-1007-CP

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. Parametric Studies of Transonic Aeroelastic Effects of an Aircraft Wing/Tip Store;Journal of Aircraft;2005-01

2. Design Studies of Transonic Flutter and Limit-Cycle Oscillation of an Aircraft Wing/Tip Store;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07

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