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035   $a(CKB)5470000002526581
035   $a(OCoLC)1284802668
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100   $a20211108j196701    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of a method of estimating high temperature low cycle fatigue behavior of materials /$fby G.R. Halford and S.S. Manson
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$d[January 1967].
215   $a1 online resource (approximately 26 pages) $cillustrations
225 1 $aNASA/TM ;$vX-52357
300   $a"Technical paper proposed for presentation at National Metal Congress sponsored by the American Society for Metals Cleveland, Ohio, October 19, 1967."
320   $aIncludes bibliographical references (pages 8-10).
606   $aFatigue (materials)$2nasat
606   $aCreep rupture strength$2nasat
606   $aTemperature effects$2nasat
615  7$aFatigue (materials)
615  7$aCreep rupture strength.
615  7$aTemperature effects.
700   $aHalford$b Gary R.$01139998
702   $aManson$b S. S.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910716961403321
996   $aApplication of a method of estimating high temperature low cycle fatigue behavior of materials$93512949
997   $aUNINA