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Assessment of low cycle fatigue crack growth under mixed-mode loading conditions by using a cohesive zone model
Affiliation:1. Department of Mechanical Engineering, University of Wuppertal, Germany;2. Tsinghua University, School of Aerospace Engineering, Peking, China;1. Structural Methods and Allowables Group, The Boeing Company. Everett, WA 98204, United States;2. Dept of Mechanical and Aerospace Engineering, University of Miami, Coral Gables, FL 33124, United States;1. Jiangsu Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, 29 Yudao St, Nanjing, Jiangsu, China;2. Research and Innovation Center, Ford Motor Company, 2101 Village Rd, Dearborn, MI, USA;3. College of Engineering and Computer Science, University of Michigan-Dearborn, 4901 Evergreen Road, Dearborn, MI, USA;1. Department of Construction and Manufacturing Engineering, University of Oviedo, Gijón 33203, Spain;2. Department of Mechanical Engineering, Technical University of Denmark, DK-2800 Kgs. Lyngby, Denmark;1. AMADE, Universitat de Girona, Campus Montilivi s/n, 17003 Girona, Spain;1. Faculdade de Engenharia da Universidade do Porto, Departamento de Engenharia Mecânica, Rua Dr. Roberto Frias, 4200-465 Porto, Portugal;2. IBM T.J. Watson Research Center, 1101 Kitchawan Road, Yorktown Heights, NY 10598, USA
Abstract:
Keywords:Cyclic cohesive zone model (CCZM)  Damage evolution  Low cycle fatigue (LCF)  Elastoplastic rupture  Finite plastic zone
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