02006oam 2200589 450 991070987710332120180725083926.0(CKB)5470000002473483(OCoLC)785108338(EXLCZ)99547000000247348320120408j198806 ua 0engurbn||||||abptxtrdacontentcrdamediacrrdacarrierAeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /George T. Carson, Jr., and Milton LambWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Division,June 1988.1 online resource (171 pages) illustrationsNASA/TP ;2814"June 1988."Prepared at Langley Research Center.Includes bibliographical references (page 13).Nozzle geometrynasatMach numbernasatHypersonic nozzlesnasatRamjet enginesnasatNozzle efficiencynasatJet nozzlesTestingJet nozzlesTestingfastNozzle geometry.Mach number.Hypersonic nozzles.Ramjet engines.Nozzle efficiency.Jet nozzlesTesting.Jet nozzlesTesting.Carson George T.1397663Lamb MiltonUnited States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQGPOBOOK9910709877103321Aeropropulsive characteristics of isolated combined turbojet3459640UNINA