Experimental Study of Splitter Plates for Use with Semispan Wing Models
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
2. Rensselaer Polytechnic Institute
3. University of Washington, Seattle
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1227
Reference14 articles.
1. Experimental Investigation of Semispan Model Testing Techniques
2. Malik, A. and Render, P.M. "Use of Wall Suction in Half Model Wind Tunnel Testing," AIAA Paper 2010-4828.
3. Experimental and Numerical Investigation of a Wing-Body Junction Flow
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