Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [electronic resource] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / Anthony Neal Watkins ... [and others]

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Bibliographic Details
Online Access:	Online Access Online Access
Corporate Author:	Langley Research Center
Other Authors:	Watkins, Anthony Neal
Format:	Government Document Electronic eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Series:	NASA technical memorandum ; 217316.
Subjects:	Pressure measurement. Pressure sensitive paints. Flow distribution. Flight simulation. Pressure sensors. Horizontal flight. Blade tips.

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Online Access
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Call Number:	NAS 1.15:2011-217316
NAS 1.15:2011-217316	Available