Modification of Transonic Blowdown Wind Tunnel to Produce Oscillating Freestream Mach Number
Author:
Affiliation:
1. Ohio State University, Columbus, Ohio 43235
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051090
Reference22 articles.
1. Harmonic optimization of a periodic flow wind tunnel
2. The Effect of Varying Freestream Velocity on Airfoil Dynamic Stall Characteristics
3. Combined translation/pitch motion - A new airfoil dynamic stall simulation
4. Dynamic Stall Due to Fluctuations of Velocity and Incidence
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