02174oam 2200601 a 450 991070153770332120120822083322.0(CKB)5470000002419712(OCoLC)785925432(EXLCZ)99547000000241971220120417d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierComputational analysis of a low-boom supersonic inlet[electronic resource] /Rodrick V. ChimaCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2011]1 online resource (14 pages) color illustrationsNASA/TM ;2011-217223Title from title screen (viewed on Apr. 17, 2012)."November 2011.""Prepared for the 29th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics, Honolulu, Hawaii, June 27-30, 2011.""AIAA-2011-3801."Includes bibliographical references (pages 13-14).Computational fluid dynamicsnasatEngine inletsnasatSupersonic aircraftnasatSupersonic inletsnasatInlet airframe configurationsnasatOverpressurenasatSupersonic flownasatSonic boomsnasatWind tunnel testsnasatComputational fluid dynamics.Engine inlets.Supersonic aircraft.Supersonic inlets.Inlet airframe configurations.Overpressure.Supersonic flow.Sonic booms.Wind tunnel tests.Chima Rodrick V1393796NASA Glenn Research Center.AIAA Applied Aerodynamics Conference(29th :2011 :Honolulu, Hawaii)GPOGPOGPOBOOK9910701537703321Computational analysis of a low-boom supersonic inlet3523558UNINA