LEADER 01827oam  2200577I  450 
001 9910706190803321
005 20170817144703.0
035   $a(CKB)5470000002454515
035   $a(OCoLC)858270750
035   $a(EXLCZ)995470000002454515
100   $a20130912j199812    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFracture analysis of the FAA/NASA wide stiffened panels /$fB.R. Seshadri [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1998.
215   $a1 online resource (19 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208976
300   $a"December 1998."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 17-19).
606   $aStructural analysis$2nasat
606   $aFracturing$2nasat
606   $aPanels$2nasat
606   $aStiffness$2nasat
606   $aApplications programs (computers)$2nasat
606   $aPlane strain$2nasat
606   $aCracks$2nasat
606   $aFracture mechanics$2nasat
615  7$aStructural analysis.
615  7$aFracturing.
615  7$aPanels.
615  7$aStiffness.
615  7$aApplications programs (computers)
615  7$aPlane strain.
615  7$aCracks.
615  7$aFracture mechanics.
700   $aSeshadri$b B. R.$01395565
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706190803321
996   $aFracture analysis of the FAA$93546181
997   $aUNINA