NASA NTRS · 20010072399
Langley 16- Ft. Transonic Tunnel Pressure Sensitive Paint System
Abstract
This report describes the NASA Langley 16-Ft. Transonic Tunnel Pressure Sensitive Paint (PSP) System and presents results of a test conducted June 22-23, 2000 in the tunnel to validate the PSP system. The PSP system provides global surface pressure measurements on wind tunnel models. The system was developed and installed by PSP Team personnel of the Instrumentation Systems Development Branch and the Advanced Measurement and Diagnostics Branch. A discussion of the results of the validation test follows a description of the system and a description of the test.
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Sprinkle, Danny R., Obara, Clifford J., Amer, Tahani R., Leighty, Bradley D., Carmine, Michael T., Sealey, Bradley S., Burkett, Cecil G.. 2001-06-01. Langley 16- Ft. Transonic Tunnel Pressure Sensitive Paint System. https://ntrs.nasa.gov/citations/20010072399
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