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Laser shock peening in aircraft applications and its effect on fatigue life of 7075-T7351 aluminium alloy
(2019)
Diplomityö
Diplomityö
Fatigue and other failure mechanisms, such as corrosion and stress corrosion cracking, are severe problems in metallic aircraft components. Many surface treatment methods exist to enhance the service life of metallic ...
Modelling methods for calculating fatigue stresses from simulated tire loads
(2022)
Diplomityö
Diplomityö
The purpose of this work is to determine the most practical way to determine the stresses in the drill rig from simulated tire loads. The tire loads are measured from rigid body driving simulation of the rig and the stress ...