Criteria for self loosening of fasteners under vibration

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 January 1973


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.


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

Download as .RIS




Copyright © 1973, MCB UP Limited

Please note you might not have access to this content

You may be able to access this content by login via Shibboleth, Open Athens or with your Emerald account.
If you would like to contact us about accessing this content, click the button and fill out the form.
To rent this content from Deepdyve, please click the button.