LEADER 01735oam  2200493   450 
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035   $a(CKB)5470000002509712
035   $a(OCoLC)1233179499
035   $a(OCoLC)995470000002509712
035   $a(EXLCZ)995470000002509712
100   $a20210128j202004    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEvaluation of fatigue damage accumulation functions for delamination initiation and propagation /$fCarlos G. Da?vila [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2020.
215   $a1 online resource (ii, 32 pages, 1 unnumbered page) $ccolor illustrations
225 1 $aNASA/TP ;$v2020-220584
300   $a"April 2020."
320   $aIncludes bibliographical references (pages 31-32).
606   $aComposite materials$xDelamination
606   $aComposite materials$xDelamination$2fast
606   $aCrack propagation$2nasat
606   $aFatigue life$2nasat
606   $aCyclic loads$2nasat
615  0$aComposite materials$xDelamination.
615  7$aComposite materials$xDelamination.
615  7$aCrack propagation.
615  7$aFatigue life.
615  7$aCyclic loads.
700   $aDavila$b Carlos G.$01412406
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910715231403321
996   $aEvaluation of fatigue damage accumulation functions for delamination initiation and propagation$93522076
997   $aUNINA