Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch
Author:
Publisher
Gruppo Italiano Frattura
Subject
Mechanical Engineering,Mechanics of Materials
Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. FRACTURE ANALYSIS OF REPAIRING CRACKED AIRCRAFT STRUCTURE;Journal of Theoretical and Applied Mechanics;2024-07-12
2. New investigation of delamination using the VCCT method to predict the damage in bonded composite repair plates subjected to tensile load;International Journal of Structural Integrity;2024-01-04
3. NUMERICAL STUDY OF MECHANICAL BEHAVIOR OF REPAIRED INCLINED CRACKED UNDER COMPLEX SHEAR-SHEAR LOAD: PERFORMANCE AND DURABILITY OF ALUMINUM 2024-T3 PLATE;Journal of the Serbian Society for Computational Mechanics;2023-12-01
4. NUMERICAL AND ANALYTICAL PREDICTION OF THE PROPAGATION OF DELAMINATION OF BONDED COMPOSITE REPAIR PLATES UNDER MECHANICAL LOADING;Journal of the Serbian Society for Computational Mechanics;2023-12-01
5. Study of the Behavior of the AL 2017-A Aluminium Plate Corroded and with Horizontal Cracks Treated by the Technique of Composite Materials;Advances in Materials Science;2023-06-01
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