01761nam 2200493I 450 991070278070332120141117142716.0(CKB)5470000002430389(OCoLC)895678631(EXLCZ)99547000000243038920141117j201307 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAeroelastic analyses of the SemiSpan Supersonic Transport (S⁴T) wind tunnel model at Mach 0.95 /Jiyoung HurHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,July 2014.1 online resource (64 pages) color illustrationsNASA/CR ;2014-218287Title from title screen (viewed Nov. 17, 2014)."July 2014."Includes bibliographical references (page 11).Aeroelastic analyses of the SemiSpan Supersonic Transport AeroelasticitynasatDynamic pressurenasatFlutternasatTransonic flownasatStructured grids (mathematics)nasatDynamic structural analysisnasatAeroelasticity.Dynamic pressure.Flutter.Transonic flow.Structured grids (mathematics)Dynamic structural analysis.Hur Jiyoung1385956Langley Research Center,GPOGPOBOOK9910702780703321Aeroelastic analyses of the SemiSpan Supersonic Transport (S⁴T) wind tunnel model at Mach 0.953434469UNINA