Acoustic Emission-Based Methodology to Evaluate Delamination Crack Growth Under Quasi-static and Fatigue Loading Conditions

被引:24
作者
Saeedifar, Milad [1 ,2 ]
Najafabadi, Mehdi Ahmadi [1 ]
Mohammadi, Kaivan [3 ]
Fotouhi, Mohamad [4 ]
Toudeshky, Hossein Hosseini [5 ]
Mohammadi, Reza [1 ]
机构
[1] Amirkabir Univ Technol, Dept Mech Engn, Nondestruct Testing Lab, 424 Hafez Ave, Tehran 15914, Iran
[2] Delft Univ Technol, Fac Aerosp Engn, Struct Integr & Composites Grp, Delft, Netherlands
[3] Sharif Univ Technol, Dept Mech Engn, Tehran, Iran
[4] Univ West England, Dept Design & Math, Bristol BS16 1QY, Avon, England
[5] Amirkabir Univ Technol, Dept Aerosp Engn, Tehran, Iran
关键词
Quasi-static; Fatigue; Delamination; Acoustic emission; Fatigue crack growth; FRACTURE-TOUGHNESS; GLASS/EPOXY COMPOSITES; DAMAGE CLASSIFICATION; FAILURE; STRENGTH; IMPACT; PLY; IDENTIFICATION; MECHANISMS; SIMULATION;
D O I
10.1007/s10921-017-0454-0
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The aim of this study was to investigate the applicability of acoustic emission (AE) technique to evaluate delamination crack in glass/epoxy composite laminates under quasi-static and fatigue loading. To this aim, double cantilever beam specimens were subjected to mode I quasi-static and fatigue loading conditions and the generated AE signals were recorded during the tests. By analyzing the mechanical and AE results, an analytical correlation between the AE energy with the released strain energy and the crack growth was established. It was found that there is a 3rd degree polynomial correlation between the crack growth and the cumulative AE energy. Using this correlation the delamination crack growth was predicted under both the static and fatigue loading conditions. The predicted crack growth values was were in a good agreement with the visually recorded data during the tests. The results indicated that the proposed AE-based method has good applicability to evaluate the delamination crack growth under quasi-static and fatigue loading conditions, especially when the crack is embedded within the structure and could not be seen visually.
引用
收藏
页数:13
相关论文
共 48 条
[1]  
Aghazadeh Mohandesi J., MAT DES, V30, P1950
[2]   A new semi-empirical law for variable stress-ratio and mixed-mode fatigue delamination growth [J].
Allegri, G. ;
Wisnom, M. R. ;
Hallett, S. R. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2013, 48 :192-200
[3]   Dependence of fracture toughness of composite laminates on interface ply orientations and delamination growth direction [J].
Andersons, J ;
König, M .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (13-14) :2139-2152
[4]   Compression after impact strength of repaired GFRP composite laminates under repeated impact loading [J].
Andrew, J. Jefferson ;
Arumugam, V. ;
Saravanakumar, K. ;
Dhakal, H. N. ;
Santulli, C. .
COMPOSITE STRUCTURES, 2015, 133 :911-920
[5]  
[Anonymous], 2011, D611597 ASTM INT
[6]  
[Anonymous], 2007, D552801 ASTM INT
[7]  
[Anonymous], 2005, FRACTURE MECH FUNDAM
[8]   A Global Method for the Identification of Failure Modes in Fiberglass Using Acoustic Emission [J].
Arumugam, V. ;
Kumar, C. Suresh ;
Santulli, C. ;
Sarasini, E. ;
Stanley, A. Joseph .
JOURNAL OF TESTING AND EVALUATION, 2011, 39 (05) :954-966
[9]   Acoustic Emission Characterization of Failure Modes in GFRP Laminates Under Mode I Delamination [J].
Arumugam, V. ;
Sajith, S. ;
Stanley, A. Joseph .
JOURNAL OF NONDESTRUCTIVE EVALUATION, 2011, 30 (03) :213-219
[10]   Identification of fiber breakage in fiber reinforced plastic by low-amplitude filtering of acoustic emission data [J].
Ativitavas, N ;
Fowler, TJ ;
Pothisiri, T .
JOURNAL OF NONDESTRUCTIVE EVALUATION, 2004, 23 (01) :21-36