Strain energy density approach to stable crack extension under net section yielding of aircraft fuselage-Reference-Cited by-同舟云学术

Strain energy density approach to stable crack extension under net section yielding of aircraft fuselage

Published:1995-03 Issue:2 Volume:22 Page:127-137
ISSN:0167-8442
Container-title:Theoretical and Applied Fracture Mechanics
language:en
Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Jeong D.Y.,Orringer O.,Sill G.C.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference12 articles.

1. Damage tolerance in pressurized fuselages;Swift,1987

2. Fracture toughness evaluation by Rcurve methods,1973

3. Standard practice for R-curve determination;ASTM Standard E-561-8,1986

4. Aircraft accident report — Aloha Airlines, Flight 243, Boeing 737-200, N73711, near Maui, Hawaii, April 28, 1988;National Transportation Safety Board;NTSB/ AAR-89/03, PB89-910404,1989

5. Fracture and fatigue strength evaluation of multiple site damaged aircraft fuselages — curved panel testing and analysis;Samavedam;Final Report, DOT/FAA/CT-94/l0,DOT-VNTSC-FAA-93-8,1994

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