The effect of mode I and mode II overload on subsequent mode I crack propagation is studied on single edge notch specimen of Aluminum alloy. The application of overload spike during constant amplitude high cycle fatigue introduces a large plastic zone which enhances the magnitude and size of compressive residual stress field in the vicinity of the crack tip. This enhanced compressive residual stress field reduces the available crack tip driving force, thus causing a reduction in fatigue crack growth rate. It has been observed that the number of cycles to failure increases with increase in the overload application angle. The material used in the present investigation was aluminum alloy (Zn- 4.6, Mg- 1.4, Mn-0.5, Cr-0.1, Zr-0.1, Ti-0.03) havi...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
In the present paper, the fatigue crack growth retardation following a single tensile overload appli...
Present investigation involves the study of fatigue crack growth behavior of thermo-mechanically tre...
The present investigation studies the effects of a band overload (multiple overloads) on fatigue cra...
In the present work experiments were performed in Instron-8502 machine with a 250 kN load cell capac...
The effect of single-cycle overloads on the subsequent fatigue crack growth behavior of Inconel 600 ...
This article deals with the study of the overload- underload interactions effects on fatigue crack g...
© 2017 Wiley Publishing Ltd.Fatigue data are generally derived under constant-amplitude loading cond...
© 2017 Wiley Publishing Ltd.Fatigue data are generally derived under constant-amplitude loading cond...
© 2017 Wiley Publishing Ltd.Fatigue data are generally derived under constant-amplitude loading cond...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Fatigue is the most important cause of mechanical failure of engineering structures and components. ...
Abstract-The effect of single-cycle overloads on the subsequent fatigue crack growth behavior of Inc...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
In the present paper, the fatigue crack growth retardation following a single tensile overload appli...
Present investigation involves the study of fatigue crack growth behavior of thermo-mechanically tre...
The present investigation studies the effects of a band overload (multiple overloads) on fatigue cra...
In the present work experiments were performed in Instron-8502 machine with a 250 kN load cell capac...
The effect of single-cycle overloads on the subsequent fatigue crack growth behavior of Inconel 600 ...
This article deals with the study of the overload- underload interactions effects on fatigue crack g...
© 2017 Wiley Publishing Ltd.Fatigue data are generally derived under constant-amplitude loading cond...
© 2017 Wiley Publishing Ltd.Fatigue data are generally derived under constant-amplitude loading cond...
© 2017 Wiley Publishing Ltd.Fatigue data are generally derived under constant-amplitude loading cond...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Fatigue is the most important cause of mechanical failure of engineering structures and components. ...
Abstract-The effect of single-cycle overloads on the subsequent fatigue crack growth behavior of Inc...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
In the present paper, the fatigue crack growth retardation following a single tensile overload appli...