LEADER 02124nam  2200517Ia 450 
001 9910701779103321
005 20120515091415.0
035   $a(CKB)5470000002420304
035   $a(OCoLC)793599684
035   $a(EXLCZ)995470000002420304
100   $a20120515d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aDeployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight$b[electronic resource] $epreliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel /$fAnthony Neal Watkins ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (18 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-217316
300   $aTitle from title screen (viewed on May 15, 2012).
300   $a"December 2011."
320   $aIncludes bibliographical references (pages 17-18).
517   $aDeployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight 
606   $aPressure measurement$2nasat
606   $aPressure sensitive paints$2nasat
606   $aFlow distribution$2nasat
606   $aFlight simulation$2nasat
606   $aPressure sensors$2nasat
606   $aHorizontal flight$2nasat
606   $aBlade tips$2nasat
615  7$aPressure measurement.
615  7$aPressure sensitive paints.
615  7$aFlow distribution.
615  7$aFlight simulation.
615  7$aPressure sensors.
615  7$aHorizontal flight.
615  7$aBlade tips.
701   $aWatkins$b Anthony Neal$01407931
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701779103321
996   $aDeployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight$93490472
997   $aUNINA