For reasons stated bolted connections on aircraft develop play and resultant backlash may impair safety of craft; author seeks to determine connection between stress range, load cycles and increase in play for normal eyebolt so that part can be replaced when it has reached statistical endurance limit. Brief English abstract from Luftfahrtforschung v 19 n 4 May 6 1942.
Development of play in bolted joints under fatigue
Aircraft Production
Aircraft Production ; 4 , n 47 ; p 578
1942
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Spectrum fatigue of composite bolted joints
Tema Archiv | 2002
|Fatigue and traction in friction grip bolted joints
TIBKAT | 1966
|A Study to Predict Fatigue Limits of Bolted Joints under Transverse Vibration
SAE Technical Papers | 2010
|A study of loosening and fatigue of bolted joints under transverse vibration
Kraftfahrwesen | 2005
|Numerical method for fatigue life of plane bolted joints under thermal load
SAGE Publications | 2020
|