Application of pressure- and temperature-sensitive paints to high-speed flows
- 20 June 1994
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Aerodynamic assessment of an optical pressure measurement system (OPMS) by comparison with conventional pressure measurements in a high speed wind tunnelPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- A new optical pressure measurement system (OPMS)Published by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- The application of the pressure sensitive paint technique to high speed wind tunnel testing of a fighter aircraft configuration with complex store loadingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Aerodynamic applications of pressure sensitive paintAIAA Journal, 1993
- Image registration for luminescent paint applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Video luminescent barometry - The induction periodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Boundary layer transition detection by luminescence imagingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Luminescent barometry in wind tunnelsReview of Scientific Instruments, 1990
- Principles of Fluorescence SpectroscopyPublished by Springer Nature ,1983
- New technique of surface flow visualization based on oxygen quenching of fluorescenceReview of Scientific Instruments, 1980