Effect of the Model-Sidewall Connection for a Dynamic Stall Airfoil Experiment
Author:
Affiliation:
1. DLR, German Aerospace Center, 37073 Göttingen, Germany
Funder
German Government basic research financing
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference44 articles.
1. Effect of the Model-Sidewall Connection for a Static Airfoil Experiment
2. EwaldB. F. R. “Wind Tunnel Wall Correction,” AGARDograph 336, NATO/RTO, Neuilly-Sur-Seine, France, 1998.
3. Analysis of Wind Tunnel Wall Interference Effects on Subsonic Unsteady Airfoil Flows
4. Effects of Sidewall Boundary Layers in Two-Dimensional Subsonic and Transonic Wind Tunnels
5. Wall interference assessment/correction for transonic airfoil data
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