01690nam 2200493I 450 991070570580332120170711083957.0(CKB)5470000002453354(OCoLC)993430824(EXLCZ)99547000000245335420170711j201706 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierFinite element modeling and analysis of Mars entry aeroshell concept /Samee W. Ahmed, Brittney M. LaneHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,June 2017.1 online resource (75 pages) color illustrationsNASA/TM ;2017-219374"June 2017.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 53).AerodynamicsnasatAeroshellsnasatAtmospheric entrynasatFinite element methodnasatLift drag rationasatMars atmospherenasatAerodynamics.Aeroshells.Atmospheric entry.Finite element method.Lift drag ratio.Mars atmosphere.Ahmed Samee W.1409093Lane Brittney M.Langley Research Center,GPOGPOBOOK9910705705803321Finite element modeling and analysis of Mars entry aeroshell concept3494647UNINA