01993nam 2200529I 450 991070717850332120160420133300.0(CKB)5470000002461710(OCoLC)946998844(EXLCZ)99547000000246171020160420j199608 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierMinimum weight design of a generic axisymmetric inlet /Shari-Beth NadellCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,August 1996.1 online resource (13 pages) illustrationsNASA technical memorandum ;107288Title from title screen (viewed April 20, 2016)."Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (page 9).SymmetrynasatAir intakesnasatFinite element methodnasatSupersonic inletsnasatStructural designnasatStructural weightnasatEngine designnasatSymmetry.Air intakes.Finite element method.Supersonic inlets.Structural design.Structural weight.Engine design.Nadell Shari-Beth1411929Lewis Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707178503321Minimum weight design of a generic axisymmetric inlet3504167UNINA