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SBIR/STTR

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

Completed Technology Project

Project Introduction

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. More »

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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.

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