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:

Pt. 1:
Pt. 2:
Pt. 3:
Pt. 4:

Available Online