Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches-Reference-Cited by-同舟云学术

Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches

Published:1997-10 Issue:1 Volume:28 Page:13-28
ISSN:0167-8442
Container-title:Theoretical and Applied Fracture Mechanics
language:en
Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Naboulsi S.,Mall S.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference11 articles.

1. Analysis of cracked aluminum plates repaired with bonded composite patches;Sun;AIAA J.,1996

2. Modeling of cracked metallic structure with bonded composite patch using three layer technique;Naboulsi;Compos. Struct.,1996

3. Thermal effects on adhesively bonded composite patch repair of cracked aluminum panels;Naboulsi;Theor. Appl. Fracture Mech.,1996

4. Characterization of fatigue crack growth in bonded structures-crack growth prediction in bonded structures;Ratwani;Air Force Flight Dynamics Laboratory AFFADL-TR-77-31,1977

5. Characterization of fatigue crack growth in bonded structures-analysis of cracked bonded structures;Ratwani;Air Force Flight Dynamics Laboratory AFFADL-TR-31,1977

Cited by 36 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. Impact of bonding defect on the tensile response of a composite patch-repaired structure: Effect of the defect position and size;STRUCT ENG MECH;2022

3. Laminated FRP composite patch design for arresting joint fractures (Adhesion/cohesion) in resin-infilled centrally inclined V-notched Al-6061-T6 plate;Theoretical and Applied Fracture Mechanics;2022-10

4. Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch;Frattura ed Integrità Strutturale;2022-09-22

5. Experimental and Numerical Analyses of the Effects of Overload on the Fatigue Life of Aluminum Alloy Panels Repaired with Bonded Composite Patch;International Journal of Aeronautical and Space Sciences;2021-06-08