Crack patching: analysis and design

R. Jones; M. Davis; R. J. Callinan; G. D. Mallinson

doi:10.1080/03601218208907409

Crack patching: analysis and design

R. Jones, M. Davis, R. J. Callinan, G. D. Mallinson

Research output: Contribution to journal › Article › Research › peer-review

36 Citations (Scopus)

Abstract

Bonded composite patches are frequently used to retard crack growth. This repair procedure is usually referred to as crack patching. The present paper outlines the various methods for the analysis and design of fiber composite patches in thin and thick structures. As illustrative examples the repair of fatigue cracks in the wing skins of Mirage III aircraft, of surface flaws in Macchi landing wheels, and of cracks in a truss is considered.

Original language	English
Pages (from-to)	177-190
Number of pages	14
Journal	Journal of Structural Mechanics
Volume	10
Issue number	2
DOIs	https://doi.org/10.1080/03601218208907409
Publication status	Published - Jan 1982
Externally published	Yes

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10.1080/03601218208907409

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abstract = "Bonded composite patches are frequently used to retard crack growth. This repair procedure is usually referred to as crack patching. The present paper outlines the various methods for the analysis and design of fiber composite patches in thin and thick structures. As illustrative examples the repair of fatigue cracks in the wing skins of Mirage III aircraft, of surface flaws in Macchi landing wheels, and of cracks in a truss is considered.",

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Y1 - 1982/1

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AB - Bonded composite patches are frequently used to retard crack growth. This repair procedure is usually referred to as crack patching. The present paper outlines the various methods for the analysis and design of fiber composite patches in thin and thick structures. As illustrative examples the repair of fatigue cracks in the wing skins of Mirage III aircraft, of surface flaws in Macchi landing wheels, and of cracks in a truss is considered.

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Crack patching: analysis and design

Abstract

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