Effect of the stiffness ratio on the growth of repaired fatigue cracks with composite patch-Reference-Cited by-同舟云学术

Effect of the stiffness ratio on the growth of repaired fatigue cracks with composite patch

Published:2023-03-28 Issue: Volume: Page:1-19
ISSN:1539-7734
Container-title:Mechanics Based Design of Structures and Machines
language:en
Short-container-title:Mechanics Based Design of Structures and Machines

Author:

Salem M.¹,Mhamdia R.¹,Mechab B.¹,Bachir Bouiadjra B.¹²

Affiliation:

1. LMPM, Department of Mechanical Engineering, University of Sidi Bel Abbes, Sidi Bel Abbes, Algeria

2. Mechanical Engineering Department, College of Engineering, King Saud University, Riyadh, Saudi Arabia

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Condensed Matter Physics,Aerospace Engineering,Automotive Engineering,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2023.2189941

Reference35 articles.

1. Effects of adhesive disbond and thermal residual stresses on the fatigue life of cracked 2024-T3 aluminum panels repaired with a composite patch

2. Effect of load amplitude change on the fatigue life of cracked Al plate repaired with composite patch

3. Effect of the patch length on the effectiveness of one-sided bonded composite repair for aluminum panels

4. Effects of the adhesive disband on the performances of bonded composite repairs in aircraft structures

5. COMPUTATIONAL MICROSTRUCTURE-BASED ANALYSIS OF RESIDUAL STRESS EVOLUTION IN METAL-MATRIX COMPOSITE MATERIALS DURING THERMOMECHANICAL LOADING

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