The Wing Crack Model is a fracture mechanics-based failure criterion that characterizes the initiation and propagation of wing-tipped cracks under compressive stress, distinguishing itself from other damage models by explicitly accounting for shear-induced tensile cracking at microcrack tips.
29
Publications
1.2K
Citations
101
Authors
66
Institutions
Publications per year
2017–2026
16
Variants
Wing-crack Model
Parents
Publications
29
Numerical investigation of insect wing fracture behaviour
Hamed Rajabi, A. Darvizeh, Ali Shafiei et al. · Journal of Biomechanics · 2014 · 72 citations
Engineering, Computational Engineering, Mechanical Engineering +14
1–5 of 29
Authors
101
- PB
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2
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2
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2
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1–5 of 101
Institutions
66
Centre National de la Recherche Scientifique
Paris, France
3 h-index
7 publications
334 citations
Christian-Albrechts-Universität zu Kiel
Kiel, Germany
2 h-index
5 publications
204 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
3 publications
136 citations
Purdue University West Lafayette
West Lafayette, United States
2 h-index
4 publications
303 citations
Total (France)
Paris, France
2 h-index
2 publications
159 citations
Trinity College Dublin
Dublin, Ireland
2 h-index
4 publications
102 citations
Hunan University of Science and Technology
Xiangtan, China
2 h-index
7 publications
94 citations
Hohai University
Nanjing, China
1 h-index
3 publications
93 citations
1–8 of 66
Venues
- Engineering Fracture Mechanics
4 publications · 147 citations
4
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- International Journal of Rock Mechanics and Mining Sciences
3 publications · 164 citations
3
h-index
- International Journal of Solids and Structures
3 publications · 80 citations
3
h-index
- Engineering Failure Analysis
2 publications · 67 citations
2
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- International Journal of Fatigue
2 publications · 111 citations
2
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1–5