01969nam 2200493I 450 991070578240332120170908154307.0(CKB)5470000002452580(OCoLC)989980610(EXLCZ)99547000000245258020170613j199706 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierNumerical assessment of four-port through-flow wave rotor cycles with passage height variation /D.E. Paxson and Jules W. LindauCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,June 1997.1 online resource (12 pages) illustrationsNASA technical memorandum ;107490"June 1997"--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.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"Report documentation page."AIAA-97-3142."Includes bibliographical references (pages 11-12).Computational fluid dynamicsnasatFlow distributionnasatFuel consumptionnasatGas turbine enginesnasatPressure rationasatComputational fluid dynamics.Flow distribution.Fuel consumption.Gas turbine engines.Pressure ratio.Paxson Daniel E.1386438Lindau Jules W.Lewis Research Center,GPOGPOBOOK9910705782403321Numerical assessment of four-port through-flow wave rotor cycles with passage height variation3475367UNINA