LEADER 01734nam  2200529Ia 450 
001 9910698070603321
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035   $a(CKB)5470000002394295
035   $a(OCoLC)302340500
035   $a(EXLCZ)995470000002394295
100   $a20090210d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aGlobal/local stress analysis of composite panels$b[electronic resource] /$fJ.B. Ransom and N.F. Knight, Jr
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1989]
215   $a52 pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v101622
300   $aTitle from title screen (viewed Feb. 9, 2009)
300   $a"June 1989."
320   $aIncludes bibliographical references (pages 24-26).
606   $aStrains and stresses
606   $aBoundary value problems$2nasat
606   $aGraphite-epoxy composites$2nasat
606   $aPanels$2nasat
606   $aSpline functions$2nasat
606   $aStiffening$2nasat
606   $aStructural analysis$2nasat
606   $aStructural stability$2nasat
615  0$aStrains and stresses.
615  7$aBoundary value problems.
615  7$aGraphite-epoxy composites.
615  7$aPanels.
615  7$aSpline functions.
615  7$aStiffening.
615  7$aStructural analysis.
615  7$aStructural stability.
700   $aRansom$b Jonathan B$01414830
701   $aKnight$b Norman F$01402557
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910698070603321
996   $aGlobal$93515191
997   $aUNINA