Reduction of vertical tail buffet response using active control
Author:
Affiliation:
1. McDonnell Douglas Aerospace, St. Louis, Missouri 63166
2. Parks College of St. Louis University, Cahokia, Illinois 62206
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46990
Reference17 articles.
1. Unsteady flow phenomena over delta wings at high angle of attack
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