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003 OCoLC;

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006 m d f ;

008 051020s2004 dcu s f000 0 eng d;

035 a| (Sirsi) o62121708;

035 a| (OCoLC)62121708;

049 a| ERE#;

074 a| 0431-C-08 (online);

086 0 a| TD 4.2:EX 7/3/PT.1-4;

245 00 a| Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems :b| final report.;

260 a| Washington, D.C. :b| U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research,c| [2004];

300 a| 4 volumes :b| digital, PDF file.;

336 a| text2| rdacontent;

337 a| computer2| rdamedia;

338 a| unspecified2| rdacarrier;

500 a| Title from title screen (viewed on Oct. 20, 2005).;

500 a| "November 2004.";

505 0 a| 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.;

538 a| Mode of access: Internet from the FAA Hughes Technical Center web site. Addresses as of 10/20/05: http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p1.pdf (pt. 1), http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p2.pdf (pt. 2), http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p3.pdf (pt. 3) http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p4.pdf (pt. 4); current access is available via PURLs.;

650 0 a| Aircraft gas-turbinesx| Safety measuresx| Testing.=| ^A312577;

650 0 a| Airplanesx| Turbine-propeller enginesx| Impact testing.=| ^A439489;

650 0 a| Fibrous compositesx| Impact testing.=| ^A56905;

650 0 a| Ballistic fabricsx| Testing.=| ^A868656;

650 0 a| Finite element method.=| ^A49224;

710 1 a| United States.b| Federal Aviation Administration.b| Office of Aviation Research.=| ^A425061;

856 40 3| Pt. 1:u| https://purl.fdlp.gov/GPO/LPS64601;

856 40 3| Pt. 2:u| https://purl.fdlp.gov/GPO/LPS64602;

856 40 3| Pt. 3:u| https://purl.fdlp.gov/GPO/LPS64603;

856 40 3| Pt. 4:u| https://purl.fdlp.gov/GPO/LPS64605;

998 a| 1016777;

998 a| u1016777;

596 a| 1;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| MQ1787706d| 8/7/2007l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 11/10/2005x| EDOCUMENTz| JERESOURCEo| .STAFF. 0;

Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems : final report.

Other author	United States. Federal Aviation Administration. Office of Aviation Research.
Format	Electronic
Publication Info	Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [2004]
Description	4 volumes : digital, PDF file.
Supplemental Content	Pt. 1
Supplemental Content	Pt. 2
Supplemental Content	Pt. 3
Supplemental Content	Pt. 4
Subjects	Aircraft gas-turbines--Safety measures. --Testing. Airplanes--Turbine-propeller engines. --Impact testing. Fibrous composites--Impact testing. Ballistic fabrics--Testing. Finite element method.

Contents	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.
General note	Title from title screen (viewed on Oct. 20, 2005).
General note	"November 2004."
Technical details	Mode of access: Internet from the FAA Hughes Technical Center web site. Addresses as of 10/20/05: http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p1.pdf (pt. 1), http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p2.pdf (pt. 2), http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p3.pdf (pt. 3) http://www.tc.faa.gov/its/worldpac/techrpt/ar04-40p4.pdf (pt. 4); current access is available via PURLs.
GPO item number	0431-C-08 (online)
Govt. docs number	TD 4.2:EX 7/3/PT.1-4

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Library	Location	Call Number	Status	Item Actions
	Electronic Resources	Online Content Pt. 1: Pt. 2: Pt. 3: Pt. 4:	✔ Available

Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems : final report.

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