Development of Unsteady Pressure-Sensitive Paint Application on NASA Space Launch System
Author:
Affiliation:
1. NASA Ames Research Center
2. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. Calibration of the 11-By 11-Foot Transonic Wind Tunnel at the NASA Ames Research Center
2. Investigation of Cavity Flow Using Fast-Response Pressure Sensitive Paint
3. A review of pressure-sensitive paint for high-speed and unsteady aerodynamics
4. Customer Guide to Pressure-Sensitive Paint Testing at NASA Ames Unitary Plan Wind Tunnels
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1. Aeroacoustic Analysis using Dynamic Mode Decomposition of Unsteady Pressure-Sensitive Paint Measurements;AIAA SCITECH 2024 Forum;2024-01-04
2. Advancements in the Camera Setup for Unsteady Pressure Sensitive Paint at NASA Ames Research Center;AIAA SCITECH 2024 Forum;2024-01-04
3. NASA's Unsteady Pressure-Sensitive Paint Phase I Development Overview;AIAA SCITECH 2024 Forum;2024-01-04
4. Comparison of Corcos-Based and Experimentally Derived Coherence Factors for Buffet Forcing Functions;Journal of Spacecraft and Rockets;2024-01
5. Fast-Responding Pressure-Sensitive Paint Measurements of the IC3X at Mach 7.2;Aerospace;2023-10-18
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