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

Bibliographic Details
Corporate Author: United States. Federal Aviation Administration. Office of Aviation Research
Format: Government Document Book
Language:English
Published: Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [2004]
Subjects:
Aircraft gas-turbines > Safety measures > Testing.
Airplanes > Turbine-propeller engines > Impact testing.
Fibrous composites > Impact testing.
Ballistic fabrics > Testing.
Finite element method.
Online Access:Pt. 1:
Pt. 2:
Pt. 3:
Pt. 4:
Description
Item Description:Title from title screen (viewed on Oct. 20, 2005).
"November 2004."
pt. 1. DOT/FAA/AR-04/40,P1 - pt. 2. DOT/FAA/AR-04/40,P2 - pt. 3. DOT/FAA/AR-04/40,P3 - pt.4. DOT/FAA/AR-04/40,P4
Electronic resource.
Physical Description:4 volumes : digital, PDF file.
Format: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.