References
- Alten F. Grandt Jr, "Fundamentals of Structural Integrity. Damage Tolerant Design and Nondestructive Evaluation", Wiley, 2004.
- R.S. Rutledge. Evaluation, modification and damage tolerance of an in-service aircraft critical area. 25th ICAF Symposium. Rotterdam 2009.
- G.M. van Dijk, J.B. de Jonge. Introduction to a fighter aircraft loading standard for fatigue evaluation "FALSTAFF". 8th ICAF Symposium, Lozanna 1975.
- P.R. Edwards, J. Darts. Standardised fatigue loading sequences for helicopter rotors. Part I. NLR, Amsterdam.
- P.R. Edwards, J. Darts. Standardised fatigue loading sequences for helicopter rotors. Part II. NLR, Amsterdam.
- M. Wrona. Wyznaczanie profilu średniego śmigłowców Mi-24. ITWL, Sprawozdanie nr 36/31/2008. Warszawa 2008.
- A.C. Buckner. F-16 Aircraft Structural Integrity Program (ASIP) Data Processing Training Modules - APVIb Delivery Order 0302. Lockheed Martin, Fort Worth 2006
- Prof. Grigory I. Nesterenko INVESTIGATION OF MATERIAL PROPERTIES DEGRADATION IN OPERATED AIRPLANES STRUCTURES 9th Joint FAA/DoD/NASA Aging Aircraft Conference.
- R.G. Forman i inni. Fatigue Crack Growth Database for Damage Tolerance Analysis. FAA, Waszyngton 2005.
- Introduction to NASGRO practical use and advanced techniques. Southwest Research Institute, San Antonio 2008.
- S. Klimaszewski i inni. Opracowanie widm obciążeń dla skrzydła samolotu Su-22. ITWL, Sprawozdanie nr 66/31/2005, Warszawa 2005.