Experimental study on cracked steel plates with different damage levels strengthened by CFRP laminates

被引:16
作者
Hassan, Maha M. [1 ]
Shafiq, Mohamed A. [1 ]
Mourad, Sherif A. [1 ]
机构
[1] Cairo Univ, Fac Engn, Struct Engn Dept, Gamaet El Qahera St, Giza, Egypt
关键词
Carbon Fiber Reinforced Polymer (CFRP); Crack; Damage degree; Fatigue tests; Steel plates; PARIS LAW CONSTANTS; FATIGUE BEHAVIOR; PERFORMANCE; GROWTH; DELAMINATION; STRIPS;
D O I
10.1016/j.ijfatigue.2020.105914
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Strengthening steel structures using CFRP Laminates has recently attracted increasing attention. Several studies focused on the efficiency of this strengthening technique. However, little is known regarding efficiency when applied to steel plates with different levels of damage considering various strengthening schemes for loading conditions other than pure tension. In this research, fatigue behavior of cracked steel plates strengthened with CFRP laminates is experimentally investigated considering several parameters including strengthening scheme and level of damage. Samples are tested under eccentric cyclic loading and efficiency of repair is concluded. Then, a study is followed to examine reliability of available analytical models.
引用
收藏
页数:14
相关论文
共 65 条
[1]   Use of CFRP Overlays to Repair Fatigue Damage in Steel Plates under Tension Loading [J].
Alemdar, Fatih ;
Gangel, Regan ;
Matamoros, Adolfo ;
Bennett, Caroline ;
Barrett-Gonzalez, Ron ;
Rolfe, Stan ;
Liu, Hao .
JOURNAL OF COMPOSITES FOR CONSTRUCTION, 2014, 18 (04)
[2]   Effect of crack orientation on fatigue behavior of CFRP-strengthened steel plates [J].
Aljabar, N. J. ;
Zhao, X. L. ;
Al-Mahaidi, R. ;
Ghafoori, E. ;
Motavalli, M. ;
Powers, N. .
COMPOSITE STRUCTURES, 2016, 152 :295-305
[3]   Automatic procedure for evaluating the Paris Law of martensitic and austenitic stainless steels by means of thermal methods [J].
Ancona, F. ;
Palumbo, D. ;
De Finis, R. ;
Demelio, G. P. ;
Galietti, U. .
ENGINEERING FRACTURE MECHANICS, 2016, 163 :206-219
[4]  
[Anonymous], 2013, ANN BOOK ASTM STAND
[5]  
[Anonymous], 2004, E8 ASTM
[6]  
ASTM E., 1996, ANN BOOK ASTM STAND, V3, P994
[7]   Bonded composite repair of fatigue-cracked primary aircraft structure [J].
Baker, A .
COMPOSITE STRUCTURES, 1999, 47 (1-4) :431-443
[8]   Fatigue performance of tensile steel members strengthened with CFRP plates [J].
Bocciarelli, Massimiliano ;
Colombi, Pierluigi ;
Fava, Giulia ;
Poggi, Carlo .
COMPOSITE STRUCTURES, 2009, 87 (04) :334-343
[9]   Determination of the Paris law constants in round bars from beach marks on fracture surfaces [J].
Branco, R. ;
Antunes, F. V. ;
Costa, J. D. ;
Yang, Feng Peng ;
Kuang, Zhen Bang .
ENGINEERING FRACTURE MECHANICS, 2012, 96 :96-106
[10]   Determination of Paris law constants with a reverse engineering technique [J].
Branco, R. ;
Antunes, F. V. ;
Ferreira, J. A. Martins ;
Silva, J. M. .
ENGINEERING FAILURE ANALYSIS, 2009, 16 (02) :631-638