Degradation analysis on high-cycle bending fatigue for woven SiC/SiC composites based on Wiener process model

被引:15
作者
Liu, Xi [1 ]
Wang, Rongqiao [1 ,2 ]
Hu, Dianyin [2 ,3 ]
Zhang, Long [4 ]
Chen, Gaoxiang [2 ,3 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China
[3] Beihang Univ, Res Inst Aeroengine, Beijing 100191, Peoples R China
[4] China Aerodynam Res & Dev Ctr, Facil Design & Instrumentat Inst, Mianyang 621000, Sichuan, Peoples R China
基金
中国国家自然科学基金;
关键词
Degradation analysis; Composite material; Wiener process; Bending fatigue; POLYMER-MATRIX COMPOSITE; PROGRESSIVE DAMAGE; SIMULATION; FAILURE; BEHAVIOR; JOINT; LIFE;
D O I
10.1016/j.matdes.2020.109295
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A comprehensive investigation of degradation analysis under high-cycle bending fatigue (HCBF) loading for composite materials was conducted based on the Wiener process model. Degradation data are generated by conducting the probabilistic progressive damage analysis of composite materials considering the variability of material properties including mechanical properties and strength. Based on the degradation data, the Wiener process model is established with the power time transformation function and linear time-scale functions. The HCBF tests of composite cantilever beam specimen (CBS) and turbine guide vane (TGV) are conducted to evaluate the degradation process of composite materials. Compared with the experimental data and Monte Carlo simulation (MCS) method, the proposed methodology has the promising potentials to improve computational efficiency with acceptable computational accuracy for the CBSs. As for the TGV, the maximum relative errors for mean fatigue life arc within 17.89%, while the degradation tendency from experiments is similar to the simulated degradation curves, verifying the rationality of the proposed method based on Wiener process model. Moreover, reliability analysis is conducted based on the stochastic degradation process, which can be used to determine whether the performance of the structure meets the design requirement. (C) 2020 The Authors. Published by Elsevier Ltd.
引用
收藏
页数:12
相关论文
共 42 条
[1]   Effects of surface quality and loading history on fatigue life of laser-machined poly(methyl methacrylate) [J].
Abar, Farzad ;
Abadyan, Mohamadreza ;
Aghazade, Jamshid .
MATERIALS & DESIGN, 2015, 65 :473-481
[2]   Cohesive zone and level set method for simulation of high cycle fatigue delamination in composite materials [J].
Amiri-Rad, Ahmad ;
Mashayekhi, Mohammad ;
van der Meer, Frans P. .
COMPOSITE STRUCTURES, 2017, 160 :61-69
[3]  
[Anonymous], 2013, ABAQUS DOCUMENTATION
[4]  
Bansal N. P., 2005, HDB CERAMIC COMPOSIT, DOI [10.1007/b104068, DOI 10.1007/B104068]
[5]   Statistical analysis of the mechanical properties of composite materials [J].
Barbero, E ;
Fernández-Sáez, J ;
Navarro, C .
COMPOSITES PART B-ENGINEERING, 2000, 31 (05) :375-381
[6]   Prediction of progressive failure in multidirectional composite laminated panels [J].
Basu, Shiladitya ;
Waas, Anthony M. ;
Ambur, Damodar R. .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2007, 44 (09) :2648-2676
[7]   An engineering point of view about fatigue of polymer matrix composite materials [J].
Bathias, Claude .
INTERNATIONAL JOURNAL OF FATIGUE, 2006, 28 (10) :1094-1099
[8]  
Coles S., 2001, INTRO STA MODELING E
[9]   Reliability analysis for a Wiener degradation process model under changing failure thresholds [J].
Gao, Hongda ;
Cui, Lirong ;
Kong, Dejing .
RELIABILITY ENGINEERING & SYSTEM SAFETY, 2018, 171 :1-8
[10]   Progressive debonding analysis of composite blade root joint of wind turbines under fatigue loading [J].
Hosseini-Toudeshky, H. ;
Jahanmardi, M. ;
Goodarzi, M. S. .
COMPOSITE STRUCTURES, 2015, 120 :417-427