Surface hot-film method for the measurement of transition, separation and reattachment points
Author:
Affiliation:
1. Kobe Univ., Japan
2. NASA, Langley Research Center, Hampton, VA
3. McDonnell Douglas Aerospace West Co., Long Beach, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2918
Reference9 articles.
1. Determination of mean and dynamic skin friction, separation and transition in low-speed flow with a thin-film heated element
2. Transition experiments on a flat plate at subsonic and supersonic speeds
3. A transition detection study using a cryogenic hot film system in the Langley 0.3-meter transonic cryogenic tunnel
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