Fatigue properties of adhesive-bonded laminated sheet material of aluminum alloys
- 31 December 1979
- journal article
- Published by Elsevier in Engineering Fracture Mechanics
- Vol. 12 (4) , 561-579
- https://doi.org/10.1016/0013-7944(79)90098-5
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- The effect of sheet thickness on fatigue crack retardation in 2024-T3 aluminum alloyPublished by Elsevier ,2003
- Growth Characteristics of a Fatigue Crack Approaching and Growing Beneath an Adhesively Bonded DoublerJournal of Engineering Materials and Technology, 1978
- A Parametric Study of Fatigue Crack Growth Behavior in Adhesively Bonded Metallic StructuresJournal of Engineering Materials and Technology, 1978
- Fatigue Crack Propagation in 8- and 22-Layer 7075-T6 Aluminum Alloy LaminatesJournal of Engineering Materials and Technology, 1978
- Effective remote stresses and stress intensity factors for an adhesive bonded multi-ply laminateEngineering Fracture Mechanics, 1977
- Fracture Analysis of Adhesively Bonded SheetsJournal of Applied Mechanics, 1976
- Comparison of Fracture and Fatigue Properties of Clad 7075-T6 Aluminum in Monolithic and Laminated FormsPublished by SAE International ,1975
- Effect of Specimen Thickness on Delay in Fatigue Crack GrowthJournal of Testing and Evaluation, 1975
- A sandwich plate with a part-through and a debonding crackEngineering Fracture Mechanics, 1972
- Fracture Toughness of 7075-T6 and -T651 Sheet, Plate, and Multilayered Adhesive-Bonded PanelsJournal of Basic Engineering, 1967