Effects of aspect ratio and sidewall boundary-layer in airfoil testing
Author:
Affiliation:
1. Old Dominion University Research Foundation, Norfolk, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45584
Reference17 articles.
1. Similarity Rule for Sidewall Boundary Layer Effect in Two-Dimensional Wind Tunnels
2. Effects of Sidewall Boundary Layers in Two-Dimensional Subsonic and Transonic Wind Tunnels
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2. Effect of the Model-Sidewall Connection for a Static Airfoil Experiment;Journal of Aircraft;2013-03
3. Effects of aspect ratio in a transonic shock tube airfoil flow;Journal of Thermal Science;2012-09-07
4. Determination of Transonic Wind Tunnel Geometry and Studies on Wall Interference by Numerical Simulation;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
5. Theoretical Considerations of Sidewall Interference Corrections for Transonic Shock Tube Airfoil Testing;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010
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