Optical boundary-layer transition detection in a transonic wind tunnel
Author:
Affiliation:
1. Spectron Development Laboratories, Inc., Costa Mesa, CA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1430
Reference20 articles.
1. Visualization of Transition in the Flow over an Airfoil Using the Smoke-Wire Technique
2. Fancher. M. F. "Aswcts of Crvorrenics Wind _ _ Tunnel Testing Technology at Douglas,"& Paper No. 82-0606. 1982.
3. A transition detection study using a cryogenic hot film system in the Langley 0.3-meter transonic cryogenic tunnel
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