LEADER 02036nam  2200433Ka 450 
001 9910694692803321
005 20051020154249.0
035   $a(CKB)5470000002363768
035   $a(OCoLC)62121708
035   $a(EXLCZ)995470000002363768
100   $a20051020d2004      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aExplicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems$b[electronic resource] $efinal report
210  1$aWashington, D.C. :$cU.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research,$d[2004]
215   $a4 volumes $cdigital, PDF file
300   $aTitle from title screen (viewed on Oct. 20, 2005).
300   $a"November 2004."
327   $apt. 1. Static tests and modeling -- pt. 2. Ballistic impact testing -- pt. 3. Model development and simulation of experiments -- pt. 4. Model simulation for ballistic tests, engine fan blade-out, and generic engine.
517   $aExplicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems 
606   $aAircraft gas-turbines$xSafety measures$xTesting
606   $aAirplanes$xTurbine-propeller engines$xImpact testing
606   $aFibrous composites$xImpact testing
606   $aBallistic fabrics$xTesting
606   $aFinite element method
615  0$aAircraft gas-turbines$xSafety measures$xTesting.
615  0$aAirplanes$xTurbine-propeller engines$xImpact testing.
615  0$aFibrous composites$xImpact testing.
615  0$aBallistic fabrics$xTesting.
615  0$aFinite element method.
712 02$aUnited States.$bFederal Aviation Administration.$bOffice of Aviation Research.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910694692803321
996   $aExplicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems$93427336
997   $aUNINA