Pressure sensitive paint in transonic wind-tunnel testing of the F-15
- 1 January 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (1) , 109-116
- https://doi.org/10.2514/3.46910
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Data analysis techniques for pressure- and temperature-sensitive paintPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Aerodynamic measurements based on photoluminescencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Aerodynamic applications of pressure-sensitive paintPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Luminescent barometry in wind tunnelsReview of Scientific Instruments, 1990