LEADER 01758nam  2200469I  450 
001 9910708660803321
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035   $a(CKB)5470000002470617
035   $a(OCoLC)981511016
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100   $a20170405j199704    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aZIP2DL, an elastic-plastic, large-rotation finite-element stress analysis and crack-growth simulation program /$fXiaomin Deng, James C. Newman, Jr
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 1997.
215   $a1 online resource (i, 95 pages)
225 1 $aNASA technical memorandum ;$v110332
300   $a"April 1997."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 15-16).
606   $aUser manuals (computer programs)$2nasat
606   $aComputer programs$2nasat
606   $aFinite element method$2nasat
606   $aTwo dimensional models$2nasat
606   $aStress analysis$2nasat
615  7$aUser manuals (computer programs)
615  7$aComputer programs.
615  7$aFinite element method.
615  7$aTwo dimensional models.
615  7$aStress analysis.
700   $aDeng$b Xiaomin$01412337
702   $aNewman$b J. C.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910708660803321
996   $aZIP2DL, an elastic-plastic, large-rotation finite-element stress analysis and crack-growth simulation program$93505555
997   $aUNINA