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100   $a20111115j197012    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of shortening transition liner to decrease overall length of a ram induction combustor /$fby Donald F. Schultz, Porter J. Perkins, and Jerrold D. Wear
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1970.
215   $a1 online resource (18 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7021
300   $a"December 1970."
320   $aIncludes bibliographical references (pages 17-18).
606   $aTurbojet engines$2nasat
606   $aCombustion chambers$2nasat
606   $aAirplanes$xTurbojet engines$xCombustion
606   $aSmoke
606   $aCombustion$xResearch
606   $aAirplanes$xTurbojet engines$xCombustion$2fast
606   $aCombustion chambers$xTesting$2fast
606   $aCombustion$xResearch$2fast
606   $aSmoke$2fast
615  7$aTurbojet engines.
615  7$aCombustion chambers.
615  0$aAirplanes$xTurbojet engines$xCombustion.
615  0$aSmoke.
615  0$aCombustion$xResearch.
615  7$aAirplanes$xTurbojet engines$xCombustion.
615  7$aCombustion chambers$xTesting.
615  7$aCombustion$xResearch.
615  7$aSmoke.
700   $aSchultz$b Donald F.$02680
702   $aPerkins$b Porter J.
702   $aWear$b Jerrold D.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716552303321
996   $aEffect of shortening transition liner to decrease overall length of a ram induction combustor$93495894
997   $aUNINA