LEADER 01761nam  2200493I  450 
001 9910702780703321
005 20141117142716.0
035   $a(CKB)5470000002430389
035   $a(OCoLC)895678631
035   $a(EXLCZ)995470000002430389
100   $a20141117j201307    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeroelastic analyses of the SemiSpan Supersonic Transport (S?T) wind tunnel model at Mach 0.95 /$fJiyoung Hur
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJuly 2014.
215   $a1 online resource (64 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2014-218287
300   $aTitle from title screen (viewed Nov. 17, 2014).
300   $a"July 2014."
320   $aIncludes bibliographical references (page 11).
517   $aAeroelastic analyses of the SemiSpan Supersonic Transport 
606   $aAeroelasticity$2nasat
606   $aDynamic pressure$2nasat
606   $aFlutter$2nasat
606   $aTransonic flow$2nasat
606   $aStructured grids (mathematics)$2nasat
606   $aDynamic structural analysis$2nasat
615  7$aAeroelasticity.
615  7$aDynamic pressure.
615  7$aFlutter.
615  7$aTransonic flow.
615  7$aStructured grids (mathematics)
615  7$aDynamic structural analysis.
700   $aHur$b Jiyoung$01385956
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702780703321
996   $aAeroelastic analyses of the SemiSpan Supersonic Transport (S?T) wind tunnel model at Mach 0.95$93434469
997   $aUNINA