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.

• Supplemental Notes:
  • Program Information: Aviation Grants

Language

• English

Project

• Status: Completed
• Funding: $1559996.00
• Contract Numbers:

  2006-G-011

• Sponsor Organizations:

  Federal Aviation Administration

  William J. Hughes Technical Center, Atlantic City International Airport
  Atlantic City, NJ  United States  08405
• Project Managers:

  Altobelli, Donald

• 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