Finite Element Analysis of Cracking Bodies
Author:
Affiliation:
1. Boeing Military Airplane Co., Seattle, Wash.
2. University of Washington, Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.51004
Reference17 articles.
1. Application of running-crack eigenfunctions to finite-element simulation of crack propagation
2. Toward a singular element for propagating cracks
Cited by 6 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 coupled analysis method for structures with independently modelled finite element subdomains;International Journal for Numerical Methods in Engineering;1995-11-15
2. The State of the Art in Computational Dynamic Fracture Mechanics;JSME international journal. Ser. A, Mechanics and material engineering;1994-10-15
3. Coupled analysis of independently modeled finite element subdomains;33rd Structures, Structural Dynamics and Materials Conference;1992-04-13
4. Finite element solutions for propagating interface cracks with singularity elements;Engineering Fracture Mechanics;1991-01
5. The use of quarter point element in dynamic crack analysis;Engineering Fracture Mechanics;1986-01
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