A new facility and technique for two-dimensional aerodynamic testing
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44906
Reference6 articles.
1. Transonic Flow about a Thick Circular-Arc Airfoil
2. 4Sewall, W.G. "The Effects of Sidewall Boundary Layers in Two-Dimensional Subsonic and Transonic Wind Tunnels," AIAA Paper 81-1297,1981,
3. Numerical Simulation of High Reynolds Number Transonic Flows
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