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 /

Bibliographic Details

Corporate Author:	Langley Research Center
Other Authors:	Watkins, Anthony Neal
Format:	Government Document 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.
Online Access:	https://purl.fdlp.gov/GPO/gpo22695