The Development and Implementation of a Cryogenic Pressure Sensitive Paint System in the National Transonic Facility
Author:
Affiliation:
1. NASA Langley Research Center
2. ATK
3. Jacobs Technology Inc
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-421
Reference21 articles.
1. Luminescent barometry in wind tunnels
2. 2Morris, M.J., Benne, M.E., Crites, R.C., and Donovan, J.F. "Aerodynamic Measurements Based in Photoluminescence," AIAA Paper 93-0175,31stAerospaceSciencesMeetingandExhibit,Reno,Nevada,January11-14,1993.
3. Pressure-sensitive paint in aerodynamic testing
4. 4Torgerson, S., Liu, T., and Sullivan, J. "Use of Pressure Sensitive Paints in Low Speed Flows," AIAA Paper 96-2184, Advanced Measurement and GroundTestingTechnologyConference, NewOrleans, Louisiana, June 17-20,1996.
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