Abstract
This paper presents a design methodology, and the associated data base, for the damage-tolerant design of adhesively bonded repairs. This methodology is illustrated by considering repairs to an edge-cracked panel and to multi-site damage in a fuselage lap joint.
Original language | English |
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Pages (from-to) | 19-37 |
Number of pages | 19 |
Journal | Composite Structures |
Volume | 28 |
Issue number | 1 |
DOIs | |
Publication status | Published - 1 Jan 1994 |
Externally published | Yes |