Have a personal or library account? Click to login
Study of the Impact of Prolonged Operation on Residual Deformations in the Airframe Structure of an Aircraft Cover

Study of the Impact of Prolonged Operation on Residual Deformations in the Airframe Structure of an Aircraft

Open Access
|Dec 2025

References

  1. Hosford WF. Mechanical Behavior of Materials. 2nd ed. Cambridge: Cambridge University Press; 2010. 428 p. Available from: https://ceimusb.wordpress.com/wpcontent/uploads/2015/04/mechanicalbehaviorofmaterialshosford.pdf
  2. Wright JR, Cooper JE. Introduction to Aircraft Aeroelasticity and Loads. 2nd ed. 2015. 605 p. Available from: https://rexresearch1.com/AeroEngineeringLibrary/IntroAircraftAeroelasticityLoads.pdf
  3. Sticchi M, Schnubel D, Kashaev N, Huber N. Review of residual stress modification techniques for extending the fatigue life of metallic aircraft components. Appl Mech Rev. 2015;67(1):010801. doi:10.1115/1.4029896
  4. Megson THG. Aircraft Structures for Engineering Students. 4th ed. London: Butterworth-Heinemann; 2013. 804 p. Available from: https://soaneemrana.org/onewebmedia/AIRCRAFT%20STRUCTURES%20BY%20T.H.G.%20MEGSON%20%284th%20%20Edition%29.pdf
  5. Hodges DH, Pierce GA. Introduction to Structural Dynamics and Aeroelasticity. 2nd ed. Cambridge: Cambridge University Press; 2011. 247 p. Available from: https://www.cambridge.org/core/books/introduction-to-structural-dynamics-and- aeroelasticity/38F8A0FF59844464F5034E8E0EA8BD31
  6. Federal Aviation Administration. AC 25.571-1D: Damage Tolerance and Fatigue Evaluation of Structure. U.S. Department of Transportation; 2011. 41 p. Available from: https://www.faa.gov/documentLibrary/media/Advisory_Circular/AC_25_571- 1D_.pdf
  7. European Aviation Safety Agency. Certification Specifications for Large Aeroplanes CS-25. Amendment 3. 2007 Sep 19. 617 p. Available from: https://www.easa.europa.eu/sites/default/files/dfu/CS-25_Amdt%203_19.09.07_Consolidated%20version.pdf
  8. International Civil Aviation Organization. Doc 9760: Airworthiness Manual. 4th ed. 2020. 420 p. Available from: https://aviation-insight.aero/wp-content/uploads/2021/05/ICAO-9760-docs-4thEdition.pdf
  9. Ishchenko S, Tofil A. Aerodynamic behavior of aircraft caused by residual strain in wings. Proc Natl Aviat Univ. 2011;48(3):125–137.
  10. Zhu L, Sun G, Bao W, You Z, Meng F, Dong M. Structural deformation monitoring of flight vehicles based on optical fiber sensing technology: A review and future perspectives. Engineering. 2022;16:39–55. doi: 10.1016/j.eng.2021.02.022
  11. Tekhnologicheskie ukazaniia po vypolneniiu reglamentnykh rabot na samoletakh An-24, An-26, An-30 [Technological Guidelines for Performing Scheduled Maintenance on An-24, An-26, An-30 Aircraft]. Issue 27. Moscow: Air Transport Publishing House; 1992. 154 p. Available from: https://an-26.com/TU-24/25- 27/TU-27.pdf (in Russian)
  12. Instruktsiia po nivelirovaniiu I, II, III i IV klassov [Instruction for Levelling of Classes I, II, III, and IV]. Moscow: Nedra Publishing House; 1974. 160 p. Available from: https://meganorm.ru/Data2/1/4293744/4293744086.pdf (in Russian)
  13. Federal Aviation Administration. AC 120-93: Damage Tolerance Inspections for Repairs and Alterations. 2007. Available from: https://www.faa.gov/document Library/media/Advisory_Circular/AC_120-93.pdf
Language: English
Page range: 69 - 84
Submitted on: Aug 11, 2025
|
Accepted on: Nov 6, 2025
|
Published on: Dec 24, 2025
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2025 Sergii Ishchenko, Sergii Boiko, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.