References
- [1] Wanhill, R. J. H., Molent, L., Barter, S. A. and Amsterdam, E. (2015). Milestone Case Histories in Aircraft Structural Integrity. NLR-TP-2015-193 National Aerospace Laboratory NLR, Nederland.
- [2] AGARD Lecture Series 206. Aging Combat Aircraft Fleets – Long Term Applications. 1996
- [3] Barszcz, P., Borgon, J., Leski, A. and Niezgoda, T. (2002). Exemplary Applications of the Reverse Engineering Method In the Process Of Extending Service Lives Of Aircraft In Operation in the Polish Air Forces. International Design Conference – DESIGN 2002 Dubrovnik, May 14-17, pp. 605-610.
- [4] Klimaszewski, S., Kurdelski, M. and Leski, A. (2007). Aircraft structural integrity program as an practical use of fracture mechanics. Zeszyty Naukowe Politechniki Swietokrzyskiej. Nauki Techniczne. 4, pp. 58-59.
- [5] Engineering Science Data Unit ESDU Data Item No. E.07.01. Endurance of aluminium alloys.
- [6] Leski, A., Lisiecki, J. and Reymer, P. (2011). Monitorowanie obciazen eksploatacyjnych samolotow MiG-29 i MiG-29UB na podstawie analizy wartosci przeciazen pionowych (wspolczynnikow obciazenia) nz na koniec IV kwartału 2011. RAPORT Nr 141/31/2011, ITWL. (in Polish)
- [7] Damage Severity of Monitored Fatigue Load Spectra. National Aerospace Laboratory Netherlands. NLR TP 92009 U. January 1992.