Modelling of cracking sites/development in axial dovetail joints of aero-engine compressor discs

Faculty	Engineering	Year:	2006
Type of Publication:	ZU Hosted	Pages:	30-48
Authors:	Amro Shehata Mohamed Shehata Fayed Staff Zu Site Abstract In Staff Site
Journal:	International Journal of Fatigue International Journal of Fatigue	Volume:	29

Keywords :	Modelling , cracking sites/development , axial dovetail joints
Abstract:	This paper presents a methodology to predict probable sites of fretting fatigue cracking in axial dovetail joints of an aero-engine compressor. The paper attempts to tackle at once the problems of the numerical analysis of a typical loading

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