Explicit Finite-Element Analysis of 2024-T3/T351 Aluminum Material under Impact Loading for Airplane Engine Containment and Fragment Shielding-Reference-Cited by-同舟云学术

Explicit Finite-Element Analysis of 2024-T3/T351 Aluminum Material under Impact Loading for Airplane Engine Containment and Fragment Shielding

Published:2009-07 Issue:3 Volume:22 Page:287-295
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Buyuk Murat¹²³,Kan Steve¹²³,Loikkanen Matti J.¹²³

Affiliation:

1. FHWA/NHTSA National Crash Analysis Center, George Washington Univ., Washington, DC (corresponding author).

2. FHWA/NHTSA National Crash Analysis Center, George Washington Univ., Washington, DC.

3. The Boeing Company, Commercial Airplanes Division, P.O. Box 3707, Seattle, WA 98124-2207.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282009%2922%3A3%28287%29

Reference9 articles.

1. Gogolowski R. P. and Morgan B. R. (2002). “Ballistic experiments with titanium and aluminum targets.” FAA Rep. No. DOT/FAA/AR-01/21 Federal Aviation Administration Washington D.C.

2. Johnson G. R. and Cook W. H. (1983). “A constitutive model and data for metals subject to large strains high strain rates and high temperatures.” Proc. 7th Int. Symp. on Ballistics The Hague The Netherlands 541–547.

3. Kay G. (2003). “Failure modeling of titanium 6Al-4V and aluminum 2024-T3 with the Johnson–Cook material model.” FAA Rep. No. DOT/FAA/AR-03/57 Federal Aviation Administration Washington D.C.

4. Kay G. Goto D. and Couch R. (2007). “Statistical testing of aluminum titanium lexan and composites for transport airplane rotor burst fragment shielding.” FAA Rep. No. DOT/FAA/AR-07/26 Federal Aviation Administration Washington D.C.

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