LEADER 01929nam  2200517I  450 
001 9910705287903321
005 20140321134235.0
035   $a(CKB)5470000002448484
035   $a(OCoLC)874142363
035   $a(EXLCZ)995470000002448484
100   $a20140321d1983      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTransverse vibration and buckling of a cantilevered beam with tip body under constant axial base acceleration /$fby Joel Storch and Stephen Gates
210  1$aCambridge, Massachusetts :$cThe Charles Stark Draper Laboratory, Inc. ;$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$d1983.
215   $a1 online resource (iv, 58 pages) $cillustrations
225 1 $aNASA-CR ;$v175567
225 1 $aCSDL-R ;$v1675
300   $aTitle from title screen (viewed on Mar. 21, 2014).
300   $a"October 1983."
320   $aIncludes bibliographical references (page 58).
606   $aDeformation$2nasat
606   $aEuler buckling$2nasat
606   $aMechanical properties$2nasat
606   $aPartial differential equations$2nasat
606   $aSteady state creep$2nasat
606   $aStress analysis$2nasat
615  7$aDeformation.
615  7$aEuler buckling.
615  7$aMechanical properties.
615  7$aPartial differential equations.
615  7$aSteady state creep.
615  7$aStress analysis.
700   $aStorch$b Joel$01391130
702   $aGates$b Stephen
712 02$aCharles Stark Draper Laboratory,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705287903321
996   $aTransverse vibration and buckling of a cantilevered beam with tip body under constant axial base acceleration$93477385
997   $aUNINA