Vortical flow field investigation using the pressure sensitive paint technique at low speed
Author:
Affiliation:
1. Mitsubishi Heavy Industries, Ltd., Nagoya, Japan
2. NASA, Ames Research Center, Moffett Field, CA
3. Stanford Univ., CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-388
Reference12 articles.
1. Surface pressure field mapping using luminescent coatings
2. Lecture series 1993-05;Crites R. C.
3. Torgerson S. D., Liu T. ,Sullivan J. P., Use of Pressure Sensitive Paints in LowSpeed Flows, AIAA 96-2184
4. CelikZ.Z. and Roberts L., Vortical Flow Control on aDelta Wing by Lateral Blowing, AIAA 94-0509
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2. Pressure Measurement Systems;Springer Handbook of Experimental Fluid Mechanics;2007
3. Surface pressure measurements by using pressure-sensitive paints;Aerospace Science and Technology;2005-06
4. Pressure-Correction Method for Low-Speed Pressure-Sensitive Paint Measurements;AIAA Journal;2003-05
5. Quantitative visualization of the leading-edge vortices on a delta wing by using pressure-sensitive paint;Journal of Visualization;2001-06
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