Deployment of a Pressure Sensitive Paint System for Measuring Global Surface Pressures on Rotorcraft Blades in Simulated Forward Flight
Author:
Affiliation:
1. NASA Langley Research Center
2. Army Joint Programs Office
3. ATK
4. Innovative Scientific Solutions, Inc.
5. Ohio State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2756
Reference29 articles.
1. Measurement Around a Rotor Blade Excited in Pitch, Part 2: Unsteady Surface Pressure
2. Laser Velocimetry and Blade Pressure Measurements of a Blade‐Vortex Interaction
3. Luminescent barometry in wind tunnels
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4. Measuring Surface Pressures on Rotor Blades Using Pressure-Sensitive Paint;AIAA Journal;2016-01
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