Criteria for self loosening of fasteners under vibration

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 January 1973

Abstract

This is the continuation of the article by Gerhard H. Junker, of the European Research and Engineering Standard Pressed Steel Co, Unbrako. The first part, which appeared in October, covered the mechanism of self loosening. The E‐F‐N curves, surface integrity and test programme will be covered in the final part of this feature.

Citation

JUNKER, G. (1973), "Criteria for self loosening of fasteners under vibration", Aircraft Engineering and Aerospace Technology, Vol. 45 No. 1, pp. 12-17. https://doi.org/10.1108/eb034981

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Publisher

:

MCB UP Ltd

Copyright © 1973, MCB UP Limited

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