Roll-Yaw Control at High Angle of Attack by Forebody Tangential Blowing
Author:
Affiliation:
1. EMBRAER, Sao Jose dos Campos 12225, Brazil
2. Stanford University, Stanford, California 94305-4035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2261
Reference17 articles.
1. Alleviation of Vortex-Induced Asymmetric Loads
2. Forebody vortex management for yaw control at high angles of attack
3. Active control of wing rock using tangential leading-edge blowing
4. Water-tunnel investigation of dynamic manipulation of forebody vortices
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