Fatigue crack growth rate properties are typically determined by experimental methods in accordance with ASTM Standard E647. These traditional methods use standard notched specimens that are precracked under cyclic tensile loads before the main test. The data that are produced using this approach have been demonstrated elsewhere to be potentially adversely affected by the test method, particularly in the threshold region where load reduction (LR) methods are also required. Coarse‐grained materials that exhibit rough and tortuous fatigue surfaces have been observed to be strongly affected by the tensile precracking and LR, in part because the anomalies caused by crack closure and roughness‐induced closure become more important. The focus of ...
The purpose of the research is to apply the modified Hartman-Schijve equation for predicting small c...
The fatigue behaviour of circumferentially notched specimens made of titanium alloy, Ti-6Al-4V, has ...
An experimental study is conducted to examine the crack tip/microstructure interactions in lamellar ...
Reliable prediction of fatigue crack growth rates in aerospace materials and components underpins th...
This thesis investigates fatigue crack growth rate behavior in the threshold and near-threshold regi...
In this paper we present an overview of experimental and modelling studies of fatigue crack growth r...
Crack closure is an important factor affecting fatigue crack growth in high strength alloy materials...
The growth behavior of naturally-initiated small cracks in single edge notched tensile (SENT) specim...
A titanium alloy (Ti-6Al-4V STOA) plate material was provided by the University of Dayton Research I...
abstract: Widespread knowledge of fracture mechanics is mostly based on previous models that general...
This study deals with the influence of microstructure on the fatigue crack growth resistance of ^...
AbstractThe fatigue crack growth modeling that based on linear fracture mechanics under the Mode I c...
An investigation was performed to study the effects of slip character and crack closure on the propa...
The loading frequency effects on elevated temperature fatigue crack growth behavior in a new near-α,...
Some materials such as 7050-T7451 and beta-annealed Ti-6Al-4V exhibit very rough fatigue crack surfa...
The purpose of the research is to apply the modified Hartman-Schijve equation for predicting small c...
The fatigue behaviour of circumferentially notched specimens made of titanium alloy, Ti-6Al-4V, has ...
An experimental study is conducted to examine the crack tip/microstructure interactions in lamellar ...
Reliable prediction of fatigue crack growth rates in aerospace materials and components underpins th...
This thesis investigates fatigue crack growth rate behavior in the threshold and near-threshold regi...
In this paper we present an overview of experimental and modelling studies of fatigue crack growth r...
Crack closure is an important factor affecting fatigue crack growth in high strength alloy materials...
The growth behavior of naturally-initiated small cracks in single edge notched tensile (SENT) specim...
A titanium alloy (Ti-6Al-4V STOA) plate material was provided by the University of Dayton Research I...
abstract: Widespread knowledge of fracture mechanics is mostly based on previous models that general...
This study deals with the influence of microstructure on the fatigue crack growth resistance of ^...
AbstractThe fatigue crack growth modeling that based on linear fracture mechanics under the Mode I c...
An investigation was performed to study the effects of slip character and crack closure on the propa...
The loading frequency effects on elevated temperature fatigue crack growth behavior in a new near-α,...
Some materials such as 7050-T7451 and beta-annealed Ti-6Al-4V exhibit very rough fatigue crack surfa...
The purpose of the research is to apply the modified Hartman-Schijve equation for predicting small c...
The fatigue behaviour of circumferentially notched specimens made of titanium alloy, Ti-6Al-4V, has ...
An experimental study is conducted to examine the crack tip/microstructure interactions in lamellar ...