Click on the DOI link below to access the article (may not be free).The purpose of this study was to determine the effect of dents on the stable crack growth in 0.04-in.-thick 2024-T3 bare aluminum sheet. The test specimens were either pristine, dented, or reworked. The edge-cracked pin-loaded specimens of 8 in. in width were tested at constant-amplitude loading with a stress ratio of 0.2, producing stable crack growth aldose to 4 in. completely through two dents on the crack line. Dents were produced with a drop tower having a 0.5 in. spherical hardened-steel indenter head. Dent depths ranged from 0.03 to 0.0325 in., measured on the convex side of the specimen. A starter notch of 0.3 in. was produced at the edge of the specimen with a jewe...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
The paper presents the attempt to predict fatigue crack growth rate in a component subjected to vari...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering"Dec...
The present paper is concerned with the application of a "plasticity-induced" crack closur...
While it is well known that fatigue crack growth in metals that display confined slip, such as high ...
The fatigue crack growth behavior under constant amplitude and under single overload of 2024 aluminu...
The primary focus of this study was to evaluate the effects of notches and multiaxial nominal stress...
In the present investigation aluminium Alclad 2024-T3 sheet material was tested. The aim of this inv...
Fatigue is a gradual process of local strength reduction. It is a phenomenon of damage accumulation ...
One of the most vulnerable areas for the initiation and propagation of fatigue cracks in aircraft st...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The paper describes an experimental study of notch root fatigue crack growth under FALSTAFF spectrum...
Recent experimental findings are challenging today’s conventional view on the rate-controlling proce...
The paper deals with the problem of fatigue crack propagation from notches in plates made of FeP04 s...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
The paper presents the attempt to predict fatigue crack growth rate in a component subjected to vari...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering"Dec...
The present paper is concerned with the application of a "plasticity-induced" crack closur...
While it is well known that fatigue crack growth in metals that display confined slip, such as high ...
The fatigue crack growth behavior under constant amplitude and under single overload of 2024 aluminu...
The primary focus of this study was to evaluate the effects of notches and multiaxial nominal stress...
In the present investigation aluminium Alclad 2024-T3 sheet material was tested. The aim of this inv...
Fatigue is a gradual process of local strength reduction. It is a phenomenon of damage accumulation ...
One of the most vulnerable areas for the initiation and propagation of fatigue cracks in aircraft st...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The paper describes an experimental study of notch root fatigue crack growth under FALSTAFF spectrum...
Recent experimental findings are challenging today’s conventional view on the rate-controlling proce...
The paper deals with the problem of fatigue crack propagation from notches in plates made of FeP04 s...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
The paper presents the attempt to predict fatigue crack growth rate in a component subjected to vari...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...