In the present paper, the fatigue crack growth retardation following a single tensile overload applied to the 8090 alloy is studied and compared with results obtained from conventional aluminium alloys. The 8090 alloy exhibits a high retardation effect to overloads ; reasons for this good behaviour are given considering mechanical and fractographic aspects
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Der Einfluss periodischer Überlasten auf die Rissausbreitung wurde an je einer fein- und grobkörnige...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Present investigation involves the study of fatigue crack growth behavior of thermo-mechanically tre...
This study analyses the fatigue crack growth behaviour in thin AlMgSi1-T6 aluminium alloy sheets und...
AbstractThis paper presents a review of available evidence of higher than expected crack growth rate...
Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly...
Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
AbstractThis paper reports on a study on the effect of upscaling on the fatigue crack growth resista...
In this investigation variation of cyclic loading effect on fatigue crack growth is the studied. Thi...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
Abstract-The effect of single-cycle overloads on the subsequent fatigue crack growth behavior of Inc...
This article deals with the study of the overload- underload interactions effects on fatigue crack g...
Thesis (M.Eng. Sc.)--University of Adelaide, Dept. of Mechanical Engineering, 199
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Der Einfluss periodischer Überlasten auf die Rissausbreitung wurde an je einer fein- und grobkörnige...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Present investigation involves the study of fatigue crack growth behavior of thermo-mechanically tre...
This study analyses the fatigue crack growth behaviour in thin AlMgSi1-T6 aluminium alloy sheets und...
AbstractThis paper presents a review of available evidence of higher than expected crack growth rate...
Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly...
Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
AbstractThis paper reports on a study on the effect of upscaling on the fatigue crack growth resista...
In this investigation variation of cyclic loading effect on fatigue crack growth is the studied. Thi...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
Abstract-The effect of single-cycle overloads on the subsequent fatigue crack growth behavior of Inc...
This article deals with the study of the overload- underload interactions effects on fatigue crack g...
Thesis (M.Eng. Sc.)--University of Adelaide, Dept. of Mechanical Engineering, 199
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
Der Einfluss periodischer Überlasten auf die Rissausbreitung wurde an je einer fein- und grobkörnige...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
DOI
Add to ORKG