Effects of Pressure-Sensitive Paint on Experimentally Measured Wing Forces and Pressures
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1860
Reference39 articles.
1. Pressure-sensitive paint in aerodynamic testing
2. SURFACE PRESSURE MEASUREMENTS USING LUMINESCENT COATINGS
3. 4Schlichting, H., Boundary-Layer Theory, 6th ed.McGraw-Hill, New York, 1968, pp.596-623.
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