02103oam 2200565 450 991070743770332120160825123208.0(CKB)5470000002465153(OCoLC)761335595(EXLCZ)99547000000246515320111115j198103 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPerformance of semi-transpiration-cooled liner in high-temperature-rise combustor /Jerrold D. Wear, Arthur M. Trout and John M. Smith[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,March 1981.1 online resource (17 pages) illustrationsNASA technical paper ;1806Title from title screen (viewed on Aug. 25, 2016)."March 1981.""Performing Organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (page 17).Combustion efficiencynasatFuel injectionnasatFuel-air rationasatStoichiometrynasatThermodynamic efficiencynasatCombustion efficiency.Fuel injection.Fuel-air ratio.Stoichiometry.Thermodynamic efficiency.Wear Jerrold D.1386080Trout Arthur M.Smith John M(John Milton),1922-Lewis Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910707437703321Performance of semi-transpiration-cooled liner in high-temperature-rise combustor3465241UNINA