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100   $a20120408j198806    ua             0
101 0 $aeng
135   $aurbn||||||abp
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /$fGeorge T. Carson, Jr., and Milton Lamb
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Division,$dJune 1988.
215   $a1 online resource (171 pages) $cillustrations
225 1 $aNASA/TP ;$v2814
300   $a"June 1988."
300   $aPrepared at Langley Research Center.
320   $aIncludes bibliographical references (page 13).
606   $aNozzle geometry$2nasat
606   $aMach number$2nasat
606   $aHypersonic nozzles$2nasat
606   $aRamjet engines$2nasat
606   $aNozzle efficiency$2nasat
606   $aJet nozzles$xTesting
606   $aJet nozzles$xTesting$2fast
615  7$aNozzle geometry.
615  7$aMach number.
615  7$aHypersonic nozzles.
615  7$aRamjet engines.
615  7$aNozzle efficiency.
615  0$aJet nozzles$xTesting.
615  7$aJet nozzles$xTesting.
700   $aCarson$b George T.$01397663
702   $aLamb$b Milton
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709877103321
996   $aAeropropulsive characteristics of isolated combined turbojet$93459640
997   $aUNINA