Computations of vortex-breakdown induced tail buffet undergoing bending and torsional vibrations-Reference-Cited by-同舟云学术

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Computations of vortex-breakdown induced tail buffet undergoing bending and torsional vibrations

Published:1994-04-18 Issue: Volume: Page:
ISSN:
Container-title:35th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Kandil Osama¹,Massey Steven¹,Kandil Hamdy¹

Affiliation:

1. Old Dominion Univ., Norfolk, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1428

Reference30 articles.

1. VORTEX CONTROL FOR TAIL BUFFET ALLEVIATION ON A TWIN-TAIL FIGHTER CONFIGURATION

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2. Prediction of Vertical Tail Buffet Using CFD/CSD Coupling Method;Mathematical Problems in Engineering;2021-11-23

3. Buffeting numerical simulation coupled with aerodynamics and structure based on MDDES;Science China Technological Sciences;2013-05-04

4. Airbrake-Induced Fin-Buffet Loads On Fighter Aircraft;Journal of Aircraft;2008-09

5. EFFECT OF DYNAMIC ROLLING OSCILLATIONS ON TWIN-TAIL BUFFET RESPONSE;Journal of Sound and Vibration;2002-04

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