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Adhesively Bonded Laminated Metal Structure
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English
Abstract
Adhesively bonded metallic laminates are a fabrication concept for providing fail-safe structure. This type of structure was evaluated under Air Force Contract AF33(615)-73-C-3001, “Advanced Metallic Air Vehicle Structures Program.” Development of a bonding process for large-area bonding, adhesives test data, and component test data from the program are discussed.
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Authors
Citation
Stout, R., "Adhesively Bonded Laminated Metal Structure," SAE Technical Paper 740259, 1974, https://doi.org/10.4271/740259.Also In
References
- Kaufman J. G. “Fracture Toughness of 7075-T6 and -T651 Sheet, Plate and Multilayered Adhesive-Bonded Panels.” ASME Jrl. of Basic Engineering Spetember 1967 503 507
- Cook J. Gordon J. E. “A Mechanism for the Control of Crack Propagation in All-Brittle Systems.” Ministry of Aviation England Explosives Research and Development Establishment 1965
- Reinhart T. J. Young G. Y. Air Force Materials Laboratory Cherry J. A. University of Dayton Research Institute “Laminated Adhesive Bonded Structures.”
- Little C. D. Bunting P. M. “Developments in Fracture Mechanics Technology.” Convair Aerospace Division Fort Worth, Texas December 1971
- Air Force Contract AF33(615)-73-C-3001 “Advanced Metallic Air Vehicle Structures Program.”