High Reynolds Number Transition Detection by Means of Temperature Sensitive Paint-Reference-Cited by-同舟云学术

High Reynolds Number Transition Detection by Means of Temperature Sensitive Paint

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Fey Uwe¹,Egami Yasuhiro¹,Engler Rolf¹

Affiliation:

1. Deutsches Zentrum für Luft- und Raumfahrt e.V.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-514

Reference12 articles.

1. Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescent Paint

2. 5Fey,U.,etal."TransitionDetectionbyTemperatureSensitvePaintatCryogenicTemperaturesintheEuropeanTransonic Windtunnel(ETW), 20thInternationalCongressonInstrumentationinAerospaceSimulationFacilities,ICIASFRecord, Göttingen, Germany, August 25.29.2003, pp.77- 88

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