A Method for the Determination of Fatigue Load Spectrums for Modern Combat Aircraft

A recorded flight data-representative flight test data-based approach for the development of fatigue load spectrums for modern combat aircraft is proposed,in which operation characteristics for third-generation heavy-weight combat aircraft in China are allowed for and load data from specific flight test programs and recorded in operations of aircraft fleets are used,to provide a practicable basis for creating load spectrums in the design process of future military aircraft.