Fast Responding Pressure-Sensitive Paint for Large-Scale Wind Tunnel Testing, Phase I

The proposed work focuses on implementing fast-response pressure-sensitive paint for measurements of unsteady pressure in rotorcraft applications. Significant rotorcraft problems such as dynamic stall, rotor blade loads in forward flight, and blade-vortex interaction all have significant unsteady pressure oscillations that must be resolved in order to understand the underlying physics.

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Maintainer TECHPORT SUPPORT
Last Updated July 31, 2019, 01:10 (CDT)
Created July 31, 2019, 01:10 (CDT)