The effects of stress ratio (R) and crack opening behavior on fatigue crack growth rates (da/dN) for aluminum alloy (AA) 2024-T3 were investigated using constant-delta K testing, closure measurements, and fractography. Fatigue crack growth rates were obtained for a range of delta K and stress ratios. Results show that constant delta K fatigue crack growth for R ranging from near 0 to 1 is divided into three regions. In Region 1, at low R, da/dN increases with increasing R. In Region 2, at intermediate R, fatigue crack growth rates are relatively independent of R. In Region 3, at high R, further increases in da/dN are observed with increasing R
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
Stress ratio effect on axial load fatigue and crack propagation tests on aluminum alloy sheet
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
Studies on the growth of small cracks have led to the observation that fatigue life of many engineer...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
In this paper fatigue crack growth behavior of aeronautical aluminum alloy 2024 T351 was studied. Ef...
A recently developed, rapidly solidified, powder metallurgy, dispersion strengthened aluminum alloy,...
The variation in fatigue crack closure behavior across the thickness of aluminum alloy specimens was...
The fatigue behaviour of aerospace structural components is dominated by the time to grow from a sma...
This research investigates the behavior of fatigue crack growth rate in both laboratory air and salt...
A fractographic study was performed on Al-alloy fatigue fracture surfaces produced by programmed loa...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
Stress ratio effect on axial load fatigue and crack propagation tests on aluminum alloy sheet
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
In this investigation, variation of cyclic loading effect on fatigue crack growth is studied. This s...
Studies on the growth of small cracks have led to the observation that fatigue life of many engineer...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
In this paper fatigue crack growth behavior of aeronautical aluminum alloy 2024 T351 was studied. Ef...
A recently developed, rapidly solidified, powder metallurgy, dispersion strengthened aluminum alloy,...
The variation in fatigue crack closure behavior across the thickness of aluminum alloy specimens was...
The fatigue behaviour of aerospace structural components is dominated by the time to grow from a sma...
This research investigates the behavior of fatigue crack growth rate in both laboratory air and salt...
A fractographic study was performed on Al-alloy fatigue fracture surfaces produced by programmed loa...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads we...