02056nam 2200565Ia 450 991069953980332120230902162035.0(CKB)5470000002403529(OCoLC)658189070(EXLCZ)99547000000240352920100826d1992 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPerformance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket[electronic resource] /Lynn A. Arrington and Brian D. Reed[Cleveland, Ohio] :National Aeronautics and Space Administration, Lewis Research Center,[1992?]1 online resource (20 pages) digital, PDF fileNASA technical memorandum ;105967Title from title screen (viewed Aug. 25, 2010).Includes bibliographical references (pages 8-9).NASA technical memorandum ;105967.Axisymmetric flownasatCoolantsnasatFilm coolingnasatFluid injectionnasatHydrogennasatHydrogen oxygen enginesnasatPropulsion system performancenasatReacting flownasatThree dimensional flownasatAxisymmetric flow.Coolants.Film cooling.Fluid injection.Hydrogen.Hydrogen oxygen engines.Propulsion system performance.Reacting flow.Three dimensional flow.Arrington Lynn A1386855Reed Brian D1391757Lewis Research Center.GPOGPOBOOK9910699539803321Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen3445795UNINA