Criteria for self loosening of fasteners under vibration
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article 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.H. (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
Publisher
:MCB UP Ltd
Copyright © 1973, MCB UP Limited