LEADER 01788oam  2200481I  450 
001 9910712054603321
005 20190521101950.0
035   $a(CKB)5470000002489556
035   $a(OCoLC)1091336070
035   $a(OCoLC)995470000002489556
035   $a(EXLCZ)995470000002489556
100   $a20190403j201902    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalibration of a structural finite element model for a representative inflatable space structure utilizing probabilistic methods and surrogate models /$fKaren H. Lyle and Thomas C. Jones
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 2019.
215   $a1 online resource (34 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2019-220250
300   $a"February 2019."
320   $aIncludes bibliographical references (pages 16-17).
606   $aAerodynamic brakes$2nasat
606   $aFinite element method$2nasat
606   $aMathematical models$2nasat
606   $aComputerized simulation$2nasat
606   $aCalibrating$2nasat
615  7$aAerodynamic brakes.
615  7$aFinite element method.
615  7$aMathematical models.
615  7$aComputerized simulation.
615  7$aCalibrating.
700   $aLyle$b Karen H.$01394148
702   $aJones$b Thomas C.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910712054603321
996   $aCalibration of a structural finite element model for a representative inflatable space structure utilizing probabilistic methods and surrogate models$93523432
997   $aUNINA