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Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel
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Year: 2011 Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,

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Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover
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Year: 2018 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Measuring global surface pressures on a circulation control concept using pressure sensitive paint
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Year: 2012 Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,

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Measuring global surface pressures on a circulation control concept using pressure sensitive paint
Authors: ---
Year: 2012 Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,

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Book
Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover
Authors: ---
Year: 2018 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Abstract


Book
Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel
Authors: ---
Year: 2011 Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,

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Abstract

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