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100   $a20120408j196901    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions /$fby Helmut F. Butze, Arthur M. Trout, and Harry M. Moyer
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJanuary 1969.
215   $a1 online resource (ii, 25 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4996
300   $a"January 1969."
320   $aIncludes bibliographical references (page 25).
606   $aAerodynamics$2nasat
606   $aCombustion chambers$2nasat
606   $aAerodynamics, Supersonic
606   $aAirplanes$xTurbojet engines
606   $aAerodynamics, Supersonic$2fast
606   $aAirplanes$xTurbojet engines$2fast
606   $aCombustion chambers$2fast
615  7$aAerodynamics.
615  7$aCombustion chambers.
615  0$aAerodynamics, Supersonic.
615  0$aAirplanes$xTurbojet engines.
615  7$aAerodynamics, Supersonic.
615  7$aAirplanes$xTurbojet engines.
615  7$aCombustion chambers.
700   $aButze$b Helmut F.$01413653
702   $aTrout$b Arthur M.
702   $aMoyer$b Harry M.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bTRL
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716066503321
996   $aPerformance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions$93510513
997   $aUNINA