02079nam 2200541Ia 450 991070156050332120120413152258.0(CKB)5470000002419482(OCoLC)785746353(EXLCZ)99547000000241948220120413d2011 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierAxisymmetric calculations of a low-boom inlet in a supersonic wind tunnel[electronic resource] /Rodrick V. Chima and Stefanie M. Hirt, Robert RegerCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2011]1 online resource (12 pages) illustrations (chiefly color)NASA/TM ;2011-217224Title from title screen (viewed on Mar. 19, 2012)."November 2011.""Prepared for the 29th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, June 27-30, 2011.""AIAA-2011-3800."Includes bibliographical references (pages 11-12).Supersonic inletsnasatComputational fluid dynamicsnasatMass flownasatFlight pathsnasatSupersonic aircraftnasatStabilitynasatSupersonic inlets.Computational fluid dynamics.Mass flow.Flight paths.Supersonic aircraft.Stability.Chima Rodrick V1393796Hirt Stefanie M1386037Reger Robert1393797NASA Glenn Research Center.AIAA Applied Aerodynamics Conference(29th :2011 :Honolulu, Hawaii)GPOGPOBOOK9910701560503321Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel3450327UNINA