Wing-Rock Limit Cycle Oscillation Prediction Based on Computational Fluid Dynamics-Reference-Cited by-同舟云学术

Wing-Rock Limit Cycle Oscillation Prediction Based on Computational Fluid Dynamics

Published:2008-05 Issue:3 Volume:45 Page:954-961
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Badcock K. J.¹,Woodgate M. A.¹,Allan M. R.²,Beran P. S.³

Affiliation:

1. University of Liverpool, Liverpool, England L69 3BX, United Kingdom

2. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

3. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7531

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.32812

Reference13 articles.

1. Numerical simulation of forced and free-to-roll delta-wing motions

2. Saad, A. A. "Simulation and Analysis of Wing Rock Physics for a Generic Fighter Model with Three Degrees-Of-Freedom," Ph.D. Dissertation,Air Force Institute of Technology, Wright-Patterson AirForce Base, Dayton, OH,July 2000.

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