01788oam 2200481I 450 991071205460332120190521101950.0(CKB)5470000002489556(OCoLC)1091336070(OCoLC)995470000002489556(EXLCZ)99547000000248955620190403j201902 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierCalibration of a structural finite element model for a representative inflatable space structure utilizing probabilistic methods and surrogate models /Karen H. Lyle and Thomas C. JonesHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,February 2019.1 online resource (34 pages) color illustrationsNASA/TM ;2019-220250"February 2019."Includes bibliographical references (pages 16-17).Aerodynamic brakesnasatFinite element methodnasatMathematical modelsnasatComputerized simulationnasatCalibratingnasatAerodynamic brakes.Finite element method.Mathematical models.Computerized simulation.Calibrating.Lyle Karen H.1394148Jones Thomas C.Langley Research Center,GPOGPOGPOBOOK9910712054603321Calibration of a structural finite element model for a representative inflatable space structure utilizing probabilistic methods and surrogate models3523432UNINA