LEADER 01725nam  2200469I  450 
001 9910704157203321
005 20160105164552.0
035   $a(CKB)5470000002438092
035   $a(OCoLC)933745170
035   $a(EXLCZ)995470000002438092
100   $a20160105j201509    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel /$fA. Neal Watkins [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 2015.
215   $a1 online resource (20 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218801
300   $aTitle from title screen (viewed on Jan. 5, 2016).
300   $a"September 2015."
320   $aIncludes bibliographical references (pages 18-20).
606   $aCryogenics$2nasat
606   $aPressure sensitive paints$2nasat
606   $aTemperature sensitive paints$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aLaminar flow airfoils$2nasat
615  7$aCryogenics.
615  7$aPressure sensitive paints.
615  7$aTemperature sensitive paints.
615  7$aTransonic wind tunnels.
615  7$aLaminar flow airfoils.
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   $a9910704157203321
996   $aPressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel$93490118
997   $aUNINA