Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects

Loris Molent; R. J. Callinan; R. Jones

doi:10.1016/0263-8223(89)90030-5

Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects

Loris Molent, R. J. Callinan, R. Jones

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

58 Citations (Scopus)

Abstract

This paper presents an overview of the structural aspects of the design and development of a local reinforcement designed to lower the stresses in a region of the F-111C wing pivot fitting which is prone to cracking. The stress analysis, representative specimen testing, thermal analysis and aspects of the full-scale static testing of this design are summarized.

Original language	English
Pages (from-to)	57-83
Number of pages	27
Journal	Composite Structures
Volume	11
Issue number	1
DOIs	https://doi.org/10.1016/0263-8223(89)90030-5
Publication status	Published - 1989
Externally published	Yes

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title = "Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects",

abstract = "This paper presents an overview of the structural aspects of the design and development of a local reinforcement designed to lower the stresses in a region of the F-111C wing pivot fitting which is prone to cracking. The stress analysis, representative specimen testing, thermal analysis and aspects of the full-scale static testing of this design are summarized.",

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AB - This paper presents an overview of the structural aspects of the design and development of a local reinforcement designed to lower the stresses in a region of the F-111C wing pivot fitting which is prone to cracking. The stress analysis, representative specimen testing, thermal analysis and aspects of the full-scale static testing of this design are summarized.

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Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects

Abstract

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