01980oam 2200565I 450 991071404690332120201211102023.0(CKB)5470000002507178(OCoLC)761185708(EXLCZ)99547000000250717820111115j196903 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierExploratory 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 /by Robert J. McGhee and James A. MartinWashington, D.C. :National Aeronautics and Space Administration,March 1969.1 online resource (39 pages) illustrationsNASA technical note ;D-5030"March 1969."Includes bibliographical references (page 11).Aerodynamics, SupersonicSupersonic nozzlesMach numberAerodynamics, SupersonicfastMach numberfastSupersonic nozzlesfastAerodynamics, Supersonic.Supersonic nozzles.Mach number.Aerodynamics, Supersonic.Mach number.Supersonic nozzles.McGhee Robert J.1409722Martin James A.United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQCOPGPOBOOK9910714046903321Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.03496851UNINA