Dynamic fracture analysis technique of aircraft fuselage containing damage subjected to blast-Reference-Cited by-同舟云学术

Dynamic fracture analysis technique of aircraft fuselage containing damage subjected to blast

Published:2013-08 Issue:3-4 Volume:58 Page:627-633
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Ju Jinsan,You Xiaochuan

Funder

National Program for New Century Excellent Talents in University

Foundation of National Science of China

Chinese Doctoral Fund

Publisher

Elsevier BV

Subject

Computer Science Applications,Modelling and Simulation

Reference11 articles.

1. Structural Integrity and Durability;Atluri,1997

2. Automation of global-intermediate-local analysis based on feature based modelling and the finite element alternating method;Kawai;Computer Modeling and Simulation in Engineering,1999

3. Computational strategies for fatigue crack growth in three dimensions with application to aircraft components;O’Donoghue;Engineering Fracture Mechanics,1995

4. Effect of bugling deformation on fracture analysis of aircraft panel containing damage and automation calculation;Ju,2004

5. Global–local hierarchical analysis techniques for damaged aircraft fuselage considering bulging deformation of crack;Ju;Key Engineering Materials,2006

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A new methodology to predict damage tolerance based on compliance via global-local analysis;Frattura ed Integrità Strutturale;2021-09-25

2. Stress analysis of Al2014-T6 riveted splice joint fuselage structure using finite element analysis;IOP Conference Series: Materials Science and Engineering;2018-12-19

3. Numerical simulation analysis of damage mode of concrete gravity dam under close-in explosion;KSCE Journal of Civil Engineering;2016-04-25

4. Fatigue Analysis of Forward Fuselage under Dynamic Conditions;Applied Mechanics and Materials;2015-06