02434nam 2200589Ia 450 991069965300332120230902161736.0(CKB)5470000002404406(OCoLC)704909437(EXLCZ)99547000000240440620110303d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierComputational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition[electronic resource] /John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (27 pages) illustrationsNASA/TM ;2010-216362Title from title screen (viewed on March 3, 2011)."May 2010.""AIAA-2009-7349."Includes bibliographical references (page 27)NASA technical memorandum ;216362.Computational fluid dynamics Computational fluid dynamics 241nasatData simulationnasatHypersonicsnasatStatic pressurenasatSupersonic combustion ramjet enginesnasatWind tunnel testsnasatAerodynamicsnasatBoundary layersnasatComputational fluid dynamics 241.Data simulation.Hypersonics.Static pressure.Supersonic combustion ramjet engines.Wind tunnel tests.Aerodynamics.Boundary layers.Slater John W17883Saunders John D1417796NASA Glenn Research Center.AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference(16th :2009 :Bremen, Germany)GPOGPOBOOK9910699653003321Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition3527372UNINA