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100   $a20101109d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUnified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields$b[electronic resource] /$fGary E. Erickson
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (v, 32 pages) $cillustrations
225 1 $aNASA/TM- ;$v2010-216197
300   $aTitle from title screen (viewed on Nov. 9, 2010).
300   $a"February 2010."
320   $aIncludes bibliographical references (pages 15-16)
410  0$aNASA technical memorandum ;$v216197.
606   $aAerodynamic configurations$2nasat
606   $aPressure sensitive paints$2nasat
606   $aFlow visualization$2nasat
606   $aShock waves$2nasat
606   $aStatic pressure$2nasat
606   $aLeading edges$2nasat
606   $aAngle of attack$2nasat
615  7$aAerodynamic configurations.
615  7$aPressure sensitive paints.
615  7$aFlow visualization.
615  7$aShock waves.
615  7$aStatic pressure.
615  7$aLeading edges.
615  7$aAngle of attack.
700   $aErickson$b Gary E$01403144
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697041803321
996   $aUnified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields$93519400
997   $aUNINA