Limiting Mach Number for Quantitative Pressure-Sensitive Paint Measurements
Author:
Affiliation:
1. University of California,Berkeley, Berkeley, California 94702
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.228
Reference7 articles.
1. Aerodynamic measurements based on photoluminescence
2. Pressure-sensitive paint in aerodynamic testing
3. Mendoza, D. R. “ Uncertainty Analysis of Luminescent Pressure Sensors,” Ph.D. Thesis, Mechanical Engineering Dept.Univ. of California, Berkeley, CA,Dec. 1996.
4. Uncertainty estimates for pressure sensitive paint measurements
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