1. Random load analysis as a link between operational stress measurement and fatigue life assessment;Buxbaum;Service Fatigue Loads—Monitoring, Simulation and Analysis. ASTM STP,1979
2. Fatigue and damage tolerance work during the aircraft design process. ICAF-Durability and Damage Tolerance in Aircraft Design;Jarfall,1985
3. Fatigue life prediction in the crack initiation and crack propagation stages;Heuler,1985
4. The significance of flight-simulation fatigue tests;Schijve,1985
5. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading;Newman;Methods and Models for Predicting Fatigue Crack Growth under Random Loading. ASTM STP,1981