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INTERPRETATION OF FATIGUE CRACK GROWTH IN ALUMINIUM ALLOYS UNDER PROGRAMMED BLOCK LOADING (1984)

Gabra, M. ; Bathias, C.

Oxford, UK : Blackwell Publishing Ltd

Fatigue & fracture of engineering materials & structures 7 (1984), S. 0

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ISSN: 1460-2695

Source: Blackwell Publishing Journal Backfiles 1879-2005

Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics

Notes: The effect of cycle ratio R on the crack propagation rate for two aluminium alloys is analysed. Fatigue crack growth under programmed block loading is presented, linear damage accumulation is established for some flight simulation tests. Aspects covered include microscopic and fractographic observations. The incidence of crack closure is examined and the concept of equivalent constant amplitude is applied. The agreement between predictions and test results is very promising.

Type of Medium: Electronic Resource

URL: http://dx.doi.org/10.1111/j.1460-2695.1984.tb00197.x

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