Control of vortical lift on delta wings by tangential leading-edge blowing
Author:
Affiliation:
1. Stanford University, Stanford, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45583
Reference11 articles.
1. Dynamics of air combat
2. Aerodynamic aspects of aircraft dynamics at high angles of attack
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