A study of the method for calculating fatigue damage of aircraft by using recorded load factors
27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010(2010)
Abstract
A study of the method for calculating fatigue damage of aircraft by using recorded load factors is presented in this paper. Through a systematical calculation by using 35000 hours of flight data recorded from two types of aircraft, each consisting 30 aircraft, it has been prove that this method is a powerful tool to monitor aircraft fatigue damage consumptions.
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Key words
Aircraft load,Fatigue calculation,Fatigue damage,Structural life monitoring
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