Non-linear Finite Element Analysis and Methods Development for Containment of Aircraft Engine Failure
The objective of this project is to develop and apply finite element modeling and simulation analysis methodologies for evaluation of aircraft engine containment.
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Supplemental Notes:
- Program Information: Aviation Grants
Language
- English
Project
- Status: Completed
- Funding: $1559996.00
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Contract Numbers:
2006-G-011
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Sponsor Organizations:
Federal Aviation Administration
William J. Hughes Technical Center, Atlantic City International Airport
Atlantic City, NJ United States 08405 -
Project Managers:
Altobelli, Donald
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Performing Organizations:
George Washington University, Washington DC
Department of Civil, Mechanical and Environmental Engineering
Washington, DC 20006 - Start Date: 20060802
- Expected Completion Date: 0
- Actual Completion Date: 20111214
- Source Data: RiP Project 30183
Subject/Index Terms
- TRT Terms: Finite element method; Simulation
- Uncontrolled Terms: Aircraft engines; Containment; Engine failure; Flight simulation
- Subject Areas: Aviation; Vehicles and Equipment;
Filing Info
- Accession Number: 01478847
- Record Type: Research project
- Source Agency: Department of Transportation
- Contract Numbers: 2006-G-011
- Files: RIP
- Created Date: Apr 19 2013 1:01AM