Unsteady Vortex Structure over Delta-Wing Subject to Transient Along-Core Blowing
Author:
Affiliation:
1. National Chung Hsing University, Taichung 40227, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.568
Reference22 articles.
1. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
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4. Leading-Edge-Vortex Augmentation in Compressible Flow
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