A short crack growth model for the prediction of constant amplitude fatigue life to technical crack initiation under multiaxial nonproportional loading has been proposed by Döring et. al. [1, 2]. Here, results of further work are presented which are intended to improve the model and extend its applicability to notched components. A satisfying accuracy of calculated fatigue lives is achieved. This is verified by experimental data (Hoffmeyer et. al. [3, 4]) for shouldered shafts and hollow tube specimen made of fine grained steel S460N under a variety of multiaxial non-proportional loading sequences. The correlation between the perception as stated in the model and real damage evolution is shown comparing calculated and experimentally de...
A significant portion of the fatigue life is typically spent in growth of small cracks. In addition,...
The present study is concerned with the use of the Modified Manson-Coffin Curve Method [1] to estima...
The three major issues which contribute to uncertainties in fatigue life estimations are the limited...
A short crack growth model for the prediction of constant amplitude fatigue life to technical crack ...
A short crack model originally proposed for multiaxial constant amplitude loading is extended and a...
A short crack model originally proposed for multiaxial constant amplitude loading is extended and a...
The fatigue life to initiate a crack of technical size is interpreted as a pure growth process of a ...
Commonly, basic experimental fatigue data are derived from unnotched smooth specimens. When this da...
A Short Crack Growth Model for the Prediction of Fatigue Lives under Multiaxial Nonproportional Load...
A significant part of the fatigue life is spent during short crack growth. Therefore, modelling of ...
The small crack problem in multiaxial fatigue is studied using available crack growth data from thin...
The fatigue assessment of notches under multiaxial and non-proportional service loading is challengi...
A brief overview of some important issues in multiaxial fatigue and life estimation is presented. Th...
Most of the prior studies on the prediction of fatigue lives have been limited to uniaxial loading c...
This study compares both uniaxial and multiaxial variable amplitude experimental crack growth data f...
A significant portion of the fatigue life is typically spent in growth of small cracks. In addition,...
The present study is concerned with the use of the Modified Manson-Coffin Curve Method [1] to estima...
The three major issues which contribute to uncertainties in fatigue life estimations are the limited...
A short crack growth model for the prediction of constant amplitude fatigue life to technical crack ...
A short crack model originally proposed for multiaxial constant amplitude loading is extended and a...
A short crack model originally proposed for multiaxial constant amplitude loading is extended and a...
The fatigue life to initiate a crack of technical size is interpreted as a pure growth process of a ...
Commonly, basic experimental fatigue data are derived from unnotched smooth specimens. When this da...
A Short Crack Growth Model for the Prediction of Fatigue Lives under Multiaxial Nonproportional Load...
A significant part of the fatigue life is spent during short crack growth. Therefore, modelling of ...
The small crack problem in multiaxial fatigue is studied using available crack growth data from thin...
The fatigue assessment of notches under multiaxial and non-proportional service loading is challengi...
A brief overview of some important issues in multiaxial fatigue and life estimation is presented. Th...
Most of the prior studies on the prediction of fatigue lives have been limited to uniaxial loading c...
This study compares both uniaxial and multiaxial variable amplitude experimental crack growth data f...
A significant portion of the fatigue life is typically spent in growth of small cracks. In addition,...
The present study is concerned with the use of the Modified Manson-Coffin Curve Method [1] to estima...
The three major issues which contribute to uncertainties in fatigue life estimations are the limited...