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100   $a20101007d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles$b[electronic resource] /$fRaymond S. Castner ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (10 pages) $cillustrations
225 1 $aNASA TM- ;$v2010-216259
300   $aTitle from title screen (viewed on Oct. 7, 2010).
300   $a"April 2010."
300   $a"AIAA-2009-5369."
320   $aIncludes bibliographical references (page 10)
410  0$aNASA technical memorandum ;$v216259.
606   $aWind tunnel tests$2nasat
606   $aSupersonic aircraft$2nasat
606   $aAerodynamic configurations$2nasat
606   $aLow cost$2nasat
606   $aSupersonic wind tunnels$2nasat
606   $aWind tunnel models$2nasat
606   $aSonic booms$2nasat
606   $aStatic pressure$2nasat
606   $aPressure sensors$2nasat
606   $aExhaust nozzles$2nasat
615  7$aWind tunnel tests.
615  7$aSupersonic aircraft.
615  7$aAerodynamic configurations.
615  7$aLow cost.
615  7$aSupersonic wind tunnels.
615  7$aWind tunnel models.
615  7$aSonic booms.
615  7$aStatic pressure.
615  7$aPressure sensors.
615  7$aExhaust nozzles.
700   $aCastner$b Raymond S$01392322
712 02$aNASA Glenn Research Center.
712 12$aJoint Propulsion Conference and Exhibit$d(45th :$f2009 :$eDenver, Colo.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699547103321
996   $aWind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles$93485459
997   $aUNINA