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The Influence of The Degree of the Rivet Hole Sizing on the Fatigue Life Cover

The Influence of The Degree of the Rivet Hole Sizing on the Fatigue Life

Fatigue of Aircraft Structures
Volume 2012 (2012): Issue 4 (December 2012)
By: Adam Lipski  
Open Access
|Apr 2013

References

  1. [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.
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  2. [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.
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  3. [3] Branch standard: Snap head rivet for aircraft. BN-70/1121-03 (in Polish).
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  4. [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).
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DOI: https://doi.org/10.2478/v10164-012-0057-2 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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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
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2013 Adam Lipski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

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