LEADER 01493nam  2200445   450 
001 9910706988403321
005 20180330103017.0
035   $a(CKB)5470000002459590
035   $a(OCoLC)1029874054
035   $a(EXLCZ)995470000002459590
100   $a20180330j201802    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFinite element simulations of two vertical drop tests of F-28 fuselage sections /$fKaren E. Jackson [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration,$dFebruary 2018.
215   $a1 online resource (vii, 59 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2018-219807
300   $a"February 2018."
320   $aIncludes bibliographical references (pages 56-59).
606   $aVertical flight$2nasat
606   $aFinite element method$2nasat
606   $aFuselages$2nasat
606   $aDrop tests$2nasat
606   $aFokker aircraft$2nasat
615  7$aVertical flight.
615  7$aFinite element method.
615  7$aFuselages.
615  7$aDrop tests.
615  7$aFokker aircraft.
700   $aJackson$b Karen E.$01397963
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706988403321
996   $aFinite element simulations of two vertical drop tests of F-28 fuselage sections$93493918
997   $aUNINA