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Title Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems [electronic resource] : final report.

Imprint Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [2004]


Location Call No. OPAC Message Status
 Axe Federal Documents Online  TD 4.2:EX 7/3/PT.1-4    ---  Available
Description 4 v. : digital, PDF file.
System Details Mode of access via the FAA Hughes Technical center web site.
Note Title from title screen (viewed on Oct. 20, 2005).
"November 2004."
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.
Subject Aircraft gas-turbines -- Safety measures -- Testing.
Airplanes -- Turbine-propeller engines -- Impact testing.
Fibrous composites -- Impact testing.
Ballistic fabrics -- Testing.
Finite element method.
Added Author United States. Federal Aviation Administration. Office of Aviation Research.
Gpo Item No. 0431-C-08 (online)
Sudoc No. TD 4.2:EX 7/3/PT.1-4

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