Numerical Computation of Pressure Distributions over Conical Forebody at High Angles of Attack
Author:
Affiliation:
1. Chengdu Aircraft Design Institute
2. Northwestern Polytechnical University
3. University of California, Irvine
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-1237
Reference23 articles.
1. Hunt,B.L."AsymmetricVortexForcesandWakesonSlenderBodies,"AIAAPaper,1982-1336,Aug.1982.
2. Similarity in Vortex Asymmetries over Slender Bodies and Wings
3. Sources of High Alpha Vortex Asymmetry at Zero Sideslip
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3. Computational Analysis of Conical Forebody at High Angles of Attack with Transitional Model;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
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