Analysis of Cracked, Adhesively Bonded Laminated Structures
- 1 September 1979
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (9) , 988-994
- https://doi.org/10.2514/3.61263
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- 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
- A note on the effect of lateral bending stiffness of stringers attached to a plate with a crackEngineering Fracture Mechanics, 1975
- A plate with a crack, stiffened by a partially debonded stringerEngineering Fracture Mechanics, 1974
- A hybrid‐element approach to crack problems in plane elasticityInternational Journal for Numerical Methods in Engineering, 1973
- A sandwich plate with a part-through and a debonding crackEngineering Fracture Mechanics, 1972
- Stress Distribution in Bonded Joints *Journal of Composite Materials, 1971
- Fracture Toughness of 7075-T6 and -T651 Sheet, Plate, and Multilayered Adhesive-Bonded PanelsJournal of Basic Engineering, 1967