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100   $a20120408j197108    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn improved method of collocation for the stress analysis of cracked plates with various shaped boundaries /$fby J.C. Newman, Jr
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1971.
215   $a1 online resource (approximately 47 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6376
300   $a"August 1971."
320   $aIncludes bibliographical references (pages 22-23).
606   $aNumerical analysis$2nasat
606   $aStress analysis$2nasat
606   $aCollocation$2nasat
606   $aCollocation methods$2fast
606   $aNumerical analysis$2fast
606   $aStrains and stresses$2fast
615  7$aNumerical analysis.
615  7$aStress analysis.
615  7$aCollocation.
615  7$aCollocation methods.
615  7$aNumerical analysis.
615  7$aStrains and stresses.
700   $aNewman$b J. C.$0878389
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bEGM
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910715360803321
996   $aAn improved method of collocation for the stress analysis of cracked plates with various shaped boundaries$93437587
997   $aUNINA