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100   $a20111115j196809    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of residual stress on fracture strength of AISI 301 stainless-steel and Ti-5A1-2.5Sn eli titanium cracked thin-wall cylinders /$fby Frederick D. Calfo
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968.
215   $a1 online resource (ii, 24 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4777
300   $a"September 1968."
320   $aIncludes bibliographical references (page 17).
606   $aResidual stresses
606   $aCylinders$xTesting
606   $aCylinders$xTesting$2fast
606   $aResidual stresses$2fast
615  0$aResidual stresses.
615  0$aCylinders$xTesting.
615  7$aCylinders$xTesting.
615  7$aResidual stresses.
700   $aCalfo$b Frederick D.$01416554
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715043203321
996   $aEffect of residual stress on fracture strength of AISI 301 stainless-steel and Ti-5A1-2.5Sn eli titanium cracked thin-wall cylinders$93522316
997   $aUNINA