Research Catalog

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

Title
  1. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems : final report.
Published by
  1. Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [2004]

Available online

Details

Additional authors
  1. United States. Federal Aviation Administration. Office of Aviation Research
Description
  1. 1 online resource (4 volumes)
Subject
  1. Aircraft gas-turbines -- Safety measures -- Testing
  2. Airplanes -- Turbine-propeller engines -- Impact testing
  3. Fibrous composites -- Impact testing
  4. Ballistic fabrics -- Testing
  5. Finite element method
Contents
  1. 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.
Call number
  1. GPO Internet TD 4.2:EX 7/3/PT.1-4
Note
  1. Title from title screen (viewed on October 20, 2005).
  2. "November 2004."
System details (note)
  1. 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.
Title
  1. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems : final report.
Imprint
  1. Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [2004]
Type of content
  1. text
Type of medium
  1. computer
Type of carrier
  1. online resource
System details
  1. 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.
Connect to:
  1. https://purl.fdlp.gov/GPO/LPS64601
Added author
  1. United States. Federal Aviation Administration. Office of Aviation Research.
Gpo item no.
  1. 0431-C-08 (online)
Sudoc no.
  1. TD 4.2:EX 7/3/PT.1-4
Research call number
  1. GPO Internet TD 4.2:EX 7/3/PT.1-4
View in legacy catalog