Three dimensional crack propagation through mesh-based explicit representation for arbitrarily shaped cracks using the extended finite element method

Author:

Ren Xiang,Guan Xuefei

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference59 articles.

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2. Federal Aviation Administration. U.S. Department of Transportation. AC 33.70-2 – damage tolerance of hole features in high-energy turbine. Federal Aviation Administration; 2009.

3. U.S. Nuclear Regulatory Commission. Regulatory guide RG 1.115 – protection against turbine missiles revision 2. U.S. NUCLEAR REGULATORY COMMISSION; 2012.

4. A finite element method for crack growth without remeshing;Moes;Int J Numer Methods Eng,1999

5. Modelling of stationary and growing cracks in fe framework without remeshing: a state-of-the-art review;Karihaloo;Comput Struct,2003

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