Three-Dimensional SGBEM-FEM Alternating Method for Analyzing Fatigue-Crack Growth in and the Life of Attachment Lugs-Reference-Cited by-同舟云学术

Three-Dimensional SGBEM-FEM Alternating Method for Analyzing Fatigue-Crack Growth in and the Life of Attachment Lugs

Published:2015-04 Issue:4 Volume:141 Page:04014142
ISSN:0733-9399
Container-title:Journal of Engineering Mechanics
language:en
Short-container-title:J. Eng. Mech.

Author:

Tian Longgang¹,Dong Leiting²,Phan Nam³,Atluri Satya N.⁴

Affiliation:

1. Ph.D. Candidate, Dept. of Geotechnical Engineering, College of Civil Engineering, Tongji Univ., Shanghai 200092, China.

2. Associate Professor, Dept. of Engineering Mechanics, Hohai Univ., Nanjing, Jiangsu 210098, China (corresponding author).

3. Branch Head, Structures Division, Naval Air Systems Command, Patuxent River, MD 20670.

4. Distinguished Professor, Center for Aerospace Research and Education, Univ. of California, Irvine, CA 92697.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29EM.1943-7889.0000870

Reference55 articles.

1. Atluri S. N. and Kathiresan K. (1978). “Stress analysis of typical flaws in aerospace structural components using three-dimensional hybrid displacement finite element methods.” Proc. AIAA/ASME 19th Space and Missile Defense (SMD) Conf. American Institute of Aeronautics and Astronautics (AIAA) Reston VA 340–350.

2. An assumed displacement hybrid finite element model for linear fracture mechanics

3. Application of triangular quarter-point elements as crack tip elements of power law hardening material;Barsoum R. S.;Int. J. Fract.,1976

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