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Calculation and Experimental Verification of Residual Stresses in Riveted Joints Used in an Airframe Cover

Calculation and Experimental Verification of Residual Stresses in Riveted Joints Used in an Airframe

Open Access
|Dec 2010

References

  1. Müller, R., P., G. (1995). An Experimental Investigation on the Fatigue Behavior of Fuselage Riveted Lap Joints; The Significance of the Rivet Squeeze Force, and a Comparison of 2924-T3 and Glare 3. Praca doktorska, Delft University of Technology, Universitatdrukkerij, Delft.
  2. Mruk, Z. (2008). Riveting process for specimen used in durability tests of riveted joint made with rivets closed with force control and axial strain measure. INSTRUCTION. (in polish). PZL Mielec. (Internal Report 1/DRG-6/42/2008)
  3. Skorupa, M., Skorupa, A., Machniewicz, T., Korbel, A. (2009). An Experimental Investigation on the Fatigue Performance of Riveted Lap Joints. In: M. J. Bos (Eds.), ICAF 2009, Bridging the Gap between Theory and Operational Practice. Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Nederlands, 27-29 May 2009.
  4. MSC Marc Documentation, Volume A: Theory and User Information. MSC Corp. 2008.
DOI: https://doi.org/10.2478/v10164-010-0023-9 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 23 - 36
Published on: Dec 20, 2010
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2010 Elżbieta Gadalinska, Wojciech Wronicz, Jerzy Kaniowski, Bartosz Korzeniowski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.