Development of a Highly Sensitive Temperature-Sensitive Paint for Measurements under Cryogenic Temperatures (100 - 160 K) Conditions
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0650
Reference15 articles.
1. B.T. Campbell, T. Liu, J. P. Sullivan 'Temperature Sensitive Fluorescent Paint Systems', AIAA 94-2483.
2. K. Nakakita, T. Osafune, K. Asai 'Global Heat Transfer Measurement in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint', AIAA 2003-0743.
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