02124nam 2200517Ia 450 991070177910332120120515091415.0(CKB)5470000002420304(OCoLC)793599684(EXLCZ)99547000000242030420120515d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierDeployment 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]Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (18 pages) color illustrationsNASA/TM ;2011-217316Title from title screen (viewed on May 15, 2012)."December 2011."Includes bibliographical references (pages 17-18).Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight Pressure measurementnasatPressure sensitive paintsnasatFlow distributionnasatFlight simulationnasatPressure sensorsnasatHorizontal flightnasatBlade tipsnasatPressure measurement.Pressure sensitive paints.Flow distribution.Flight simulation.Pressure sensors.Horizontal flight.Blade tips.Watkins Anthony Neal1407931Langley Research Center.GPOGPOBOOK9910701779103321Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight3490472UNINA