Studies on Vortex Flaps with Rounded Leading Edges for Supersonic Transport Configuration
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.264
Reference19 articles.
1. Effectiveness of leading-edge vortex flaps on 60 and 75 degree delta wings
2. Experimental investigation of vortex flaps on thick delta wings
3. Experimental studies of vortex flaps and vortex plates
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