Development of Unsteady-PSP Data Processing and Analysis Tools for the NASA Ames Unitary 11ft Wind Tunnel
Author:
Affiliation:
1. NASA Johnson Space Center
2. NASA Ames Research Center
3. Aerospace Computing, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Reference13 articles.
1. Evaluation of Unsteady Pressure Sensitive Paint Use for Space Launch Vehicle Buffet Determination
2. Unsteady Pressure Distribution on a Fluttering Airfoil using Motion-Capturing PSP System
3. Investigation of Cavity Flow Using Fast-Response Pressure Sensitive Paint
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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. Fast-Responding Pressure-Sensitive Paint Measurements of the IC3X at Mach 7.2;Aerospace;2023-10-18
4. Space Launch System Unsteady Forces Developed from Unsteady-Pressure-Sensitive-Paint–Based Corcos Model Parameters;Journal of Spacecraft and Rockets;2023-10-06
5. High-Speed Pressure Sensitive Paint Measurements of the Initial Concept 3.X Vehicle at Mach 7;AIAA SCITECH 2023 Forum;2023-01-19
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