LEADER 01843oam  2200541   450 
001 9910707802703321
005 20170111131807.0
035   $a(CKB)5470000002468536
035   $a(OCoLC)755031183
035   $a(EXLCZ)995470000002468536
100   $a20110929j198801    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDelamination stresses in semicircular laminated composite bars /$fWilliam L. Ko
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Division,$dJanuary 1988.
215   $a1 online resource (iii, 23 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4026
300   $a"January 1988."
300   $a"Performing organization: NASA Ames Research Center, Dryden Flight Research Facility" Report documentation page.
320   $aIncludes bibliographical references (page 15).
606   $aCurved beams$2nasat
606   $aDelaminating$2nasat
606   $aLaminates$2nasat
606   $aStress analysis$2nasat
606   $aAnisotropy$2nasat
615  7$aCurved beams.
615  7$aDelaminating.
615  7$aLaminates.
615  7$aStress analysis.
615  7$aAnisotropy.
700   $aKo$b William L.$01388928
712 02$aAmes Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Division,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707802703321
996   $aDelamination stresses in semicircular laminated composite bars$93439926
997   $aUNINA