LEADER 01601nam  2200445I  450 
001 9910706510203321
005 20171215151520.0
035   $a(CKB)5470000002457350
035   $a(OCoLC)1015382343
035   $a(EXLCZ)995470000002457350
100   $a20171215j201709    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aGuidelines for VCCT-based interlaminar fatigue and progressive failure finite element analysis /$fLyle R. Deobald [and twelve others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 2017.
215   $a1 online resource (32 unnumbered pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219663
300   $a"September 2017."
320   $aIncludes bibliographical references (pages 30-31).
606   $aAerospace industry$2nasat
606   $aFailure analysis$2nasat
606   $aFinite element method$2nasat
606   $aStructural analysis$2nasat
606   $aComposite materials$2nasat
615  7$aAerospace industry.
615  7$aFailure analysis.
615  7$aFinite element method.
615  7$aStructural analysis.
615  7$aComposite materials.
700   $aDeobald$b Lyle R.$01389975
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706510203321
996   $aGuidelines for VCCT-based interlaminar fatigue and progressive failure finite element analysis$93442177
997   $aUNINA