References
- Schijve, J., "Fatigue damage in aircraft structures, not wanted, but tolerated?", International Journal of Fatigue, Vol. 31, pp. 998-1011, 2009. https://doi.org/10.1016/j.ijfatigue.2008.05.016
- 송지호, "변동하중하의 피로파괴,"대한기계공학회지, 제 30권, 제2호, 1990
- FAR Part-25, Airworthiness standards: Transport category airplanes
- AC 25.571, Damage tolerance and fatigue evaluation of structure
- MIL-STD-1530A, Aircraft structural integrity program, Airplanes requirements
- Hoffman M. E, 2000, Hoffman P. C., "Corrosion and fatigue research - structural issues and relevance to naval aviation," International Journal of Fatigue, Vol. 23, pp. 1-10, 2001.
- AC 23-13A, Fatigue, fail-safe, and damage tolerance evaluation of metallic structure for part 23 airplanes
- MIL_A-8866, Airplane Strength and Rigidity Ground Test
- MMPDS-04, Metallic Material Design Data Acceptable to Government Procuring or Certification Agencies
- Ralphi, I. S., Ali, F., Robert, R. S. and Henry, O. F. "Metal Fatigue in Engineering,' John Wiley & Sons, Inc., 2001.
- DEF STAN 00-970, Part 1 Section 3, Leaflet 35, Fatigue, Safe-life substantiation
- 이무형, 박일경, 김성준, 안석민, "소형 항공기 엔진 마운트 구조물의 피로 건전성 평가," 한국항공운항학회지, 제 19권 제 4호, pp. 58-66, 2011.
- Walker, E. K., "The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6", ASTM-STP, pp. 462, 1970.
- Willenborg, J., Engle, R. M. and Woof, H. A., "A crack growth retardation model using an effective stress concept," AFFDL-TM-71-1-FBR, 1971.
- AC 20-107B, Composite aircraft structure
- MIL-HDBK-17, Composite materials handbook
- FAR Part-27, Airworthiness standards: Normal category rotorcraft
- FAR Part-29, Airworthiness standards: Transport category rotorcraft
- AC-27-1B, Certification of normal category rotorcraft
- AC-29-2C, Certification of transport category rotorcraft
- Kee, Y. J., Kim, S. H., Lee, H. C., Han, J. H. and Jeoung, J. K.,"Application of Flaw Tolerance Methodologies to Helicopter Rotor Blade Fatigue Life Evaluation," KSAS Spring Conference, pp. 169-174, 2011.
- Helicopter fatigue design guide, Advisory group for aerospace research and development, NATO, AGARDograph AGARD-AG-292, November 1983.