Through-thickness shape optimisation of typical double lap-joints including effects of differential thermal contraction during curing

Author:

Kaye R,Heller M

Publisher

Elsevier BV

Subject

Polymers and Plastics,General Chemical Engineering,Biomaterials

Reference11 articles.

1. Bonded Repair of Aircraft Structures,1988

2. Theoretical analysis of crack patching Chapter 5;Rose,1988

3. Shah LP, Heller M., Wang CH, Williams JF. Reduction of plate stress concentration factors due to bonded reinforcements. International Aerospace Conference 1997; 667–76.

4. Through-thickness shape optimisation of bonded repairs and lap-joints;Kaye;Int J Adhes Adhes,2002

5. Investigation of shape optimisation for the design of life extension options for an F/A-18 470 airframe bulkhead;Kaye;J Strain Anal,2000

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3. Topology Optimization of Adhesively Bonded Double Lap Joint;Advanced Structured Materials;2024

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