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The Concept of a Full Scale Fatigue Test of a Su-22 Fighter Bomber Cover

The Concept of a Full Scale Fatigue Test of a Su-22 Fighter Bomber

Open Access
|Jun 2015

References

  1. 1. I. A. Anderson, R. G. Parker, Full Scale Fatigue Test of the Pilatus PC9/A trainer aircraft, 20th ICAF Symposium, Bellevue, Washington, USA, 14-16 July 1999
  2. 2. L. Molent, S.A. Barter, P. White, B. Dixon, Damage tolerance demonstration testing for the Australian F/A-18, International Journal of Fatigue pp. 1031-1038, 24 May 200810.1016/j.ijfatigue.2008.05.009
  3. 3. R. S. Rutledge1, D. S. Backman1 and R. J. Hiscocks1, Evaluation, modification and damage tolerance of an in+service aircraft critical area, 25th ICAF Symposium, Rotterdam, 27–29 May 2009
  4. 4. S. Klimaszewski, A.Leski, J. Zurek, The Role of AFIT in the Polish Aging Military Aircraft Programs, Proceedings of 7th Joint FAA/DoD/NASA Conference on Aging Aircraft, New Orleans, 9-11 September 2003.
  5. 5. Klimaszewski S., Leski A., Dragan K., Kurdelski M. Aircraft Structural Integrity Program of Polish Su-22 Fitter. ASIP 2006 Conference, San Antonio 30.11-06.12.2006. USA, www.asipcon.com
DOI: https://doi.org/10.1515/fas-2014-0007 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 79 - 87
Published on: Jun 30, 2015
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2015 Piotr Reymer, Andrzej Leski, Wojciech Zieliński, Krzysztof Jankowski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.