02173oam 2200661 450 991071606650332120210908083152.0(CKB)5470000002517438(OCoLC)785280910(OCoLC)48181155(OCoLC)761258706(OCoLC)995470000002517438(EXLCZ)99547000000251743820120408j196901 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierPerformance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions /by Helmut F. Butze, Arthur M. Trout, and Harry M. MoyerWashington, D.C. :National Aeronautics and Space Administration,January 1969.1 online resource (ii, 25 pages) illustrationsNASA/TN ;D-4996"January 1969."Includes bibliographical references (page 25).AerodynamicsnasatCombustion chambersnasatAerodynamics, SupersonicAirplanesTurbojet enginesAerodynamics, SupersonicfastAirplanesTurbojet enginesfastCombustion chambersfastAerodynamics.Combustion chambers.Aerodynamics, Supersonic.AirplanesTurbojet engines.Aerodynamics, Supersonic.AirplanesTurbojet engines.Combustion chambers.Butze Helmut F.1413653Trout Arthur M.Moyer Harry M.United States.National Aeronautics and Space Administration,OCLCEOCLCETRLAD#OCLCQOCLCOOCLCFOCLCQCOPGPOOCLCOOCLCQGPOBOOK9910716066503321Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions3510513UNINA