00951cam0 22002893 450 SON000601520200917075143.0887743133420010312d1993 |||||ita|0103 baitaITGiambattista TiepoloI dipinti Opera completaMassimo GeminFilippo PedroccoVeneziaArsenale editrice1993550 p.ill.32 cmMonografie1001LAEC000179902001 *Monografie1Gemin, MassimoAF00010728070308877PEDROCCO, FilippoAF00020391070ITUNISOB20200917RICAUNISOBUNISOB70081040SON0006015M 102 Monografia moderna SBNM700001630SI81040ACQUISTOSpinosaUNISOBUNISOB20191001105441.020191001105451.0SpinosaGiambattista Tiepolo1674903UNISOB02036nam 2200433Ka 450 991069469280332120051020154249.0(CKB)5470000002363768(OCoLC)62121708(EXLCZ)99547000000236376820051020d2004 ua 0engtxtrdacontentcrdamediacrrdacarrierExplicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems[electronic resource] final reportWashington, D.C. :U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research,[2004]4 volumes digital, PDF fileTitle from title screen (viewed on Oct. 20, 2005)."November 2004."pt. 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.Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems Aircraft gas-turbinesSafety measuresTestingAirplanesTurbine-propeller enginesImpact testingFibrous compositesImpact testingBallistic fabricsTestingFinite element methodAircraft gas-turbinesSafety measuresTesting.AirplanesTurbine-propeller enginesImpact testing.Fibrous compositesImpact testing.Ballistic fabricsTesting.Finite element method.United States.Federal Aviation Administration.Office of Aviation Research.GPOGPOBOOK9910694692803321Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems3427336UNINA