References
- (1997). Aging of U.S. Air Force Aircraft. USA, Washington D.C.: National Academy Press. (NMAB-488-2)
- Dragan, K. (2006). In-service Flaw Detection and Quantification on the MiG-29 Composite Vertical Tail Skin. In the 9th European Conference on Non-Destructive Testing, Berlin, 25-29 Września 2006.
- Rücker, W. (2006). SAMCO Final Report 2006, Guideline for Structural Health Monitoring. Berlin: Federal Institute of Materials Research and Testing (BAM).
- Giurgiutiu, V. (2008). Structural Heath Monitoring and NDE - An Air Force Office of Scienific Research Structural Mechanics Program Perspective. In the 4th European Workshop on SHM, Kraków, July 2-4 2008, (35 - 39).
- Speckmann, H., & Henrich, R. (2004). Structural Health Monitoring (SHM) - Overview On Technologies Under Development. In the 16th WCNDT 2004 - World Conference on NDT, Canada: Montreal, August 30 - Sep 3 2004.
- Light Utility Helicopter Safety in Australia, RESEARCH PAPER BE04/73, Australian Transport Safety Bureau (ATSB), June 2004.
- Web page http://www.ntsb.gov/publictn/1996/SIR9603.pdf
- Shaniavski, A., A. (2004). Scale levels for fatigue fracture mechanisms of in-service crack growth in longerons of helicopter rotor blades. International Journal of Fracture. 128 (1), p. 17-24. DOI: 10.1023/B:FRAC.0000040960.52699.b9.
- Chronkite, J., D. (1993). Practical Application of Health and Usage Monitoring (HUMS) to Helicopter Rotor, Engine and Drive System. In the 49th Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society.
- Dragan, K. (2009). NDE activities connected with Service Life Extension of Main Rotor Blades of Polish Military Helicopters. In the 12th Aging Aircraft Conference, Kansas City, USA, 4-7 May 2009.
- Graff, K., F. (1991). Waves motion in elastic solids. New York: Dover Publications, Inc.