Fatigue reliability assessment of riveted lap joint of aircraft structures
โ Scribed by Wei Huang; Tie-Jun Wang; Y. Garbatov; C. Guedes Soares
- Book ID
- 113644891
- Publisher
- Elsevier Science
- Year
- 2012
- Tongue
- English
- Weight
- 730 KB
- Volume
- 43
- Category
- Article
- ISSN
- 0142-1123
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๐ SIMILAR VOLUMES
Solid aluminium alloy rivets are used in joints of aircraft structures. Riveting implies a squeezing process of the rivet stem with large plastic deformations to form the driven rivet head. The dimensions of the driven rivet head (diameter D and height H) depend on the applied squeeze load F sq . Hi
Results of an experimental research on the influence of several production related factors on the fatigue behaviour of simple riveted lap joint specimens under constant amplitude loading conditions are presented. The specimen geometry is representative for the longitudinal joints of the aircraft fus