LEADER 01980oam  2200565I  450 
001 9910714046903321
005 20201211102023.0
035   $a(CKB)5470000002507178
035   $a(OCoLC)761185708
035   $a(EXLCZ)995470000002507178
100   $a20111115j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0 /$fby Robert J. McGhee and James A. Martin
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (39 pages) $cillustrations
225 1 $aNASA technical note ;$vD-5030
300   $a"March 1969."
320   $aIncludes bibliographical references (page 11).
606   $aAerodynamics, Supersonic
606   $aSupersonic nozzles
606   $aMach number
606   $aAerodynamics, Supersonic$2fast
606   $aMach number$2fast
606   $aSupersonic nozzles$2fast
615  0$aAerodynamics, Supersonic.
615  0$aSupersonic nozzles.
615  0$aMach number.
615  7$aAerodynamics, Supersonic.
615  7$aMach number.
615  7$aSupersonic nozzles.
700   $aMcGhee$b Robert J.$01409722
702   $aMartin$b James A.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714046903321
996   $aExploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0$93496851
997   $aUNINA