Metallic thin-walled structures subjected to thermal-acoustic loadings will exhibit complex nonlinear response. Based on the nonlinear thermal-acoustic response analysis, the rain flow cycle counting (RFC) method was used to calculate the number of fatigue cycles. Then the Miner accumulative damage model was employed in conjunction with various mean stress models, including Morrow TFS and SWT, to predict the high cycle fatigue life. The nonlinear responses of 2024-T3 aluminum plate were obtained under band-limited Gaussian white noise loadings with pre/post-buckled temperature loadings, and the fatigue life was estimated. Analytical results show that the fatigue life of pre-buckled plate decreases with the increase of temperature, keeps going down to the lowest and undergoing persistent snap-through at the post-buckled region, and then goes up after entering intermittent snap-through region, which indicate that there exists a specific relationship between the thermal-acoustic fatigue life and nonlinear response behaviors.
机构:
Shenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R ChinaShenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R China
Sha, Yun Dong
Wei, Jing
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Shenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R ChinaShenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R China
Wei, Jing
Gao, Zhi Jun
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Shenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R ChinaShenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R China
Gao, Zhi Jun
Zhong, Hao Jie
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Shenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R ChinaShenyang Aerosp Univ, Fac Aerosp Engn, Shenyang 110136, Liaoning, Peoples R China
机构:
Department of Aircraft Maintenance Engineering,Chengdu Aeronautic PolytechnicDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
Jian WANG
Fengtong ZHAO
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机构:
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System,Shenyang AerospaceDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
Fengtong ZHAO
Yundong SHA
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机构:
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System,Shenyang AerospaceDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
Yundong SHA
Song GU
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机构:
Department of Aircraft Maintenance Engineering,Chengdu Aeronautic PolytechnicDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
机构:
Department of Aircraft Maintenance Engineering,Chengdu Aeronautic PolytechnicDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
Jian WANG
Fengtong ZHAO
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机构:
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System,Shenyang Aerospace UniversityDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
Fengtong ZHAO
Yundong SHA
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机构:
Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System,Shenyang Aerospace UniversityDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
Yundong SHA
Song GU
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机构:
Department of Aircraft Maintenance Engineering,Chengdu Aeronautic PolytechnicDepartment of Aircraft Maintenance Engineering,Chengdu Aeronautic Polytechnic
机构:
School of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
School of Mechanical and Electrical Engineering, Jiangxi New Energy Technology Institute, Jiangxi, XinyuSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Xu Z.
Xu H.
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机构:
School of Mechanical Engineering and Automation, Northeastern University, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Xu H.
Li H.
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机构:
School of Mechanical Engineering and Automation, Northeastern University, Shenyang
Key Laboratory of Aeroengine Impact Dynamics, Shenyang Engine Research Institute, Aero Engine Corporation of China, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Li H.
Wang X.
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机构:
Key Laboratory of Aeroengine Impact Dynamics, Shenyang Engine Research Institute, Aero Engine Corporation of China, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Wang X.
Zhang H.
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机构:
Key Laboratory of Aeroengine Impact Dynamics, Shenyang Engine Research Institute, Aero Engine Corporation of China, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Zhang H.
Liu Y.
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机构:
Key Laboratory of Aeroengine Impact Dynamics, Shenyang Engine Research Institute, Aero Engine Corporation of China, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Liu Y.
Sun W.
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机构:
School of Mechanical Engineering and Automation, Northeastern University, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Sun W.
Ma H.
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School of Mechanical Engineering and Automation, Northeastern University, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Ma H.
Zhao B.
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机构:
School of Mechanical Engineering and Automation, Northeastern University, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Zhao B.
Han Q.
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机构:
School of Mechanical Engineering and Automation, Northeastern University, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Han Q.
Jia P.
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机构:
School of Mechanical Engineering, Xi’an Jiaotong University, Xi’anSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Jia P.
Zhou J.
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机构:
School of Mechanical Engineering, Xi’an Jiaotong University, Xi’anSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin
Zhou J.
Wen B.
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机构:
School of Mechanical Engineering and Automation, Northeastern University, ShenyangSchool of Mechanical Engineering, Northeast Electric Power University,Jilin, Jilin