Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescent Paint
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2132
Reference16 articles.
1. High-Reynolds-Number Cryogenic Wind Tunnel
2. A transition detection study using a cryogenic hot film system in the Langley 0.3-meter transonic cryogenic tunnel
3. Transition detection studies in the cryogenic environment
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