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Fibre Composite Repairs to Damaged Structural Components

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Abstract

This paper outlines recent developments in bonded repair technology. Repairs to both metallic and composite structures are discussed, and the role of lap joint theory in the design of bonded repairs is outlined. This technology is illustrated by considering the recent repair to F111C aircraft in service with the RAAF.

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Authors and Affiliations

  1. Defence Science and Technology Organisation, Department of Defence, Aircraft Structures Division, Aeronautical Research Laboratory, Melbourne, Australia

    R. Jones & J. Paul

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  1. R. Jones
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  2. J. Paul
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Editors and Affiliations

  1. Department of Mechanical and Production Engineering, Paisley College of Technology, Scotland

    I. H. Marshall

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© 1989 Elsevier Science Publishers Ltd

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Jones, R., Paul, J. (1989). Fibre Composite Repairs to Damaged Structural Components. In: Marshall, I.H. (eds) Composite Structures 5. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-1125-3_1

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  • DOI: https://doi.org/10.1007/978-94-009-1125-3_1

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-6998-4

  • Online ISBN: 978-94-009-1125-3

  • eBook Packages: Springer Book Archive

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