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

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Format:
Book
Government document
Contributor:
United States. Federal Aviation Administration. Office of Aviation Research
Language:
English
Subjects (All):
Aircraft gas-turbines--Safety measures--Testing.
Aircraft gas-turbines.
Airplanes--Turbine-propeller engines--Impact testing.
Airplanes.
Fibrous composites--Impact testing.
Fibrous composites.
Ballistic fabrics--Testing.
Ballistic fabrics.
Finite element method.
Physical Description:
1 online resource (4 volumes)
Place of Publication:
Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [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.
Notes:
Title from title screen (viewed on October 20, 2005).
"November 2004."
OCLC:
62121708

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