5[2]R A Everett,W Elber.Damage Tolerance Issues as Related to Metallic Rotorcraft Dynamic Components[A]//Presented at the NATO/RTO Spring Symposium on Aging Systems:Application of Damage Tolerance Principles for Improved Airworthiness of Rotorcraft[C].Corfu,Greece April 21-22,1999
6[3]Lombardo D C,Fraser K F.Importance of Reliability Assessment to Helicopter Structure Component Fatigue Life Prediction[R].DSTO-TN-0462
8[9]Scott C Forth,Richard A Everett,John A Newman.A Novel Approach to Rotorcraft Damage tolerance[A]//6th Joint FAA/DoD/NASA Aging Aircraft Conference[C].2002:16-19
9[3]WILLIAM D HARRIS,TERRY LARCHUK.Application of Probabilistic Methodology in the Development of Retirement lives of Critical Dynamic Components in Rotorcraft[C]//Presented at the American Helicopter Society 55th Annual Forum.Montreal,Canada,1999:25-27.
10[4]TOULAS N,IRVING P E.ISaety Factors and Risk in usage Monitoring and fatigue Substantiation of Helicopter Components[C]//Presented at the American Helicopter Society 59th Annual Forum.Phoenix,Arizona,2003:6-8.