The Influence of The Degree of the Rivet Hole Sizing on the Fatigue Life
By: Adam Lipski
Open Access
|Apr 2013References
- [1] Larouche S. at all. (2001). Influence of Cold Working and Interference Fit on Fatigue Life of 7475-T7351 Aluminum Alloy Fastener Hole. Ed. J. Rouchon Cepadues. Design for Durability in the 21th Symposium of the International Committee on Aeronautical Fatigue, 27-29 June 2001 (pp. 681-698), Toulouse, France.
- [2] Lipski A., Mroziński S., Lis Z. (2011). Evaluation of the rivet hole sizing degree effect on the fatigue life, Journal of Polish CIMAC, Vol. 6(3), pp. 119-125.
- [3] Branch standard: Snap head rivet for aircraft. BN-70/1121-03 (in Polish).
- [4] Branch standard: Rivets for aviation-related purposes. Length selection, formed rivet heads dimensions and diameters of holes for rivets. BN-70/1120-03 (in Polish).
DOI: https://doi.org/10.2478/v10164-012-0057-2 | Journal eISSN: 2300-7591
Language: English
Page range: 64 - 69
Published on: Apr 30, 2013
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
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© 2013 Adam Lipski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.