Use of drag probe in supersonic flow
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13046
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1. Effect of acoustic excitation on the flow over a low- Re airfoil
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4. Experimental measurements in a large separation bubble due to a simulated glaze ice shape
5. Observations of Dynamic Stall Phenomena Using Liquid Crystal Coatings
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