LEADER 01641oam  2200457Ka 450 
001 9910697928003321
005 20141210065556.0
035   $a(CKB)5470000002393715
035   $a(OCoLC)299040630
035   $a(EXLCZ)995470000002393715
100   $a20090122d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputational simulation of high temperature metal matrix composites cyclic behavior$b[electronic resource] /$fC.C. Chamis, P.L.N. Murthy, and D.A. Hopkins
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$d[1989]
215   $a13 pages $cdigital, PDF file
300   $aTitle from title screen (viewed Jan. 15, 2009)
606   $aComputerized simulation$2nasat
606   $aHeat resistant alloys$2nasat
606   $aMetal matrix composites$2nasat
606   $aThermal cycling tests$2nasat
606   $aThermal degradation$2nasat
615  7$aComputerized simulation.
615  7$aHeat resistant alloys.
615  7$aMetal matrix composites.
615  7$aThermal cycling tests.
615  7$aThermal degradation.
700   $aChamis$b C. C$g(Christos C.)$0947874
701   $aMurthy$b P. L. N$01386975
701   $aHopkins$b Dale A$01124148
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910697928003321
996   $aComputational simulation of high temperature metal matrix composites cyclic behavior$93516417
997   $aUNINA