Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint
Author:
Affiliation:
1. National Aerospace Lab., Tokyo, Japan
2. Purdue Univ., West Lafayette, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2185
Reference20 articles.
1. High-Reynolds-Number Cryogenic Wind Tunnel
2. Johnson, C. B.,Carraway, D.L., Stainback, P. C., and Fancher,M.F. "ATransitionDetection Study Using a CryogenicHotFilm System intheLangley 0.3-Meter TransonicCryogenicTunnel",AIAAPaper 87-0049,Jan. 1987.
3. Gartenberg, E., Johnson, W.G., Jr., Johnson, C. B., Carraway,D.L.,andWright,R.E. "Transition Detection StudiesintheCryogenicEnvironment",AIAA Paper 90-3024, Aug. 1990.
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