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Timothy J. Harrison

RMIT University

10

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47

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Aircraft Structural Integrity: Corrosion Effects

2018
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Predicting the likely causes of early crack initiation for extruded aircraft components containing intergranular corrosion

2016 International Journal of Fatigue
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Experimental and Modeling Study of the Effect of Corrosion Pitting on Fatigue Failure Locations in Aircraft Components

2014 Advanced Materials Research
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Can pitting corrosion change the location of fatigue failures in aircraft

2014 International Journal of Fatigue
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Modelling the effects of intergranular corrosion around a fastener hole in 7075-T651 aluminium alloy

2014 Computational Materials Science
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A Demonstration using Low-kt Fatigue Specimens of a Method for Predicting the Fatigue Behaviour of Corroded Aircraft Components

2013
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Experimental Plan for the Development of Equivalent Crack Size Distributions and a Monte Carlo Model of Fatigue in Low and High-kt Specimens of Corroded AA7050-T7451

2012
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Differing microstructural properties of 7075-T6 sheet and 7075-T651 extruded aluminium alloy

2011 Procedia Engineering
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Separation control on high lift systems using vane vortex generators

2006
- Timothy J. Harrison
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