Limit cycle oscillation flight test results of a fighter with external stores

Author:

Denegri, Jr. Charles1

Affiliation:

1. USAF, SEEK EAGLE Office, Eglin AFB, FL

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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 and Development Activities in Korea;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

2. Transonic Flutter Prediction of Supersonic Jet Trainer with Various External Store Configurations;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

3. Numerical Investigation on the Aeroelastic Instability of a Complete Aircraft Model;JSME International Journal Series B;2005

4. 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

5. Adaptive reconfigurable control based on a reduced order system identification for flutter and aeroservoelastic instability suppression;19th AIAA Applied Aerodynamics Conference;2001-06-11

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