LEADER 01693nam  2200469I  450 
001 9910702505803321
005 20140930112023.0
035   $a(CKB)5470000002429125
035   $a(OCoLC)891568591
035   $a(EXLCZ)995470000002429125
100   $a20140929j201405    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplying pressure sensitive paint technology to rotor blades /$fA. Neal Watkins [and five others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 2014.
215   $a1 online resource (36 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2014-218259
300   $aTitle from title screen (viewed Sept. 29, 2014).
300   $a"May 2014."
320   $aIncludes bibliographical references (pages 34-36).
606   $aPressure sensitive paints$2nasat
606   $aHorizontal flight$2nasat
606   $aRotor blades (turbomachinery)$2nasat
606   $aRotary wing aircraft$2nasat
606   $aPressure measurement$2nasat
615  7$aPressure sensitive paints.
615  7$aHorizontal flight.
615  7$aRotor blades (turbomachinery)
615  7$aRotary wing aircraft.
615  7$aPressure measurement.
700   $aWatkins$b A. Neal$01396732
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702505803321
996   $aApplying pressure sensitive paint technology to rotor blades$93457248
997   $aUNINA