01871nam 2200505 450 991070866120332120170405145307.0(CKB)5470000002470613(OCoLC)981463550(EXLCZ)99547000000247061320170405j199706 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of high aspect ratio cooling channel designs for a rocket combustion chamber /Mary F. WadelCleveland, Ohio:National Aeronautics and Space Administration, Lewis Research Center,June 1997.1 online resource (11 pages) illustrationsNASA technical memorandum ;107473"June 1997.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center" Report documentation page."Prepared for the 33rd Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Seattle, Washington, July 6-9, 1997.""AIAA-97-2913."Includes bibliographical references (page 11).Combustion chambersnasatHigh aspect rationasatCoolingnasatChannelsnasatComputer programsnasatDesignnasatCombustion chambers.High aspect ratio.Cooling.Channels.Computer programs.Design.Wadel Mary F.1394787Lewis Research Center,GPOGPOBOOK9910708661203321Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber3530315UNINA