Add to ORKGsurvey of variability in the fatigue lives of aluminium alloy aircraft structures tested under gust and manoeuvre loadings using programmed and random sequences has shown that scatter associated with gust loading is significantly higher than that for manoeuvre loading. By contrast, there appears to be no systematic effect of loading sequence. The data have been treated both as lognormal and Weibull distributed
Tensile and fatigue testing results of D357 and B201 aluminum alloy aerospace castings reported in t...
Abstract: The paper presents comparison of three methods of fatigue life assessment related to alumi...
The paper presents comparison of three methods of fatigue life assessment related to aluminium alloy...
This paper describes an investigation to determine the scatter in fatigue performance of aluminium a...
Low cycle fatigue life and crack growth rates were analysis established for random load sequences, g...
Low cycle fatigue life and crack growth rates were analytically estimated for random load sequences,...
The fatigue properties of 2024 aluminum alloy under the influence of TWIST on the aviation load spec...
Fatigue is one of the critical design aspects with immense significance where thefatigue life of a m...
Fatigue life characteristics of aluminum alloy specimens under random load to failur
jAn investigation has been conducted to determine which combination of method of counting and type o...
Most of the structural components in real applications are subjected to variable amplitude loading. ...
Aluminium alloys remain a key airframe material, particularly for civil aircraft. In terms of fatigu...
AbstractScatter of fatigue life of a fleet is mainly caused by the variability in structures and loa...
International audienceAA2618 aeronautical aluminum alloy has been largely used in the past, especial...
This study deals with the aircraft wing analysis (numerical and experimental) which subjected to fat...
Tensile and fatigue testing results of D357 and B201 aluminum alloy aerospace castings reported in t...
Abstract: The paper presents comparison of three methods of fatigue life assessment related to alumi...
The paper presents comparison of three methods of fatigue life assessment related to aluminium alloy...
This paper describes an investigation to determine the scatter in fatigue performance of aluminium a...
Low cycle fatigue life and crack growth rates were analysis established for random load sequences, g...
Low cycle fatigue life and crack growth rates were analytically estimated for random load sequences,...
The fatigue properties of 2024 aluminum alloy under the influence of TWIST on the aviation load spec...
Fatigue is one of the critical design aspects with immense significance where thefatigue life of a m...
Fatigue life characteristics of aluminum alloy specimens under random load to failur
jAn investigation has been conducted to determine which combination of method of counting and type o...
Most of the structural components in real applications are subjected to variable amplitude loading. ...
Aluminium alloys remain a key airframe material, particularly for civil aircraft. In terms of fatigu...
AbstractScatter of fatigue life of a fleet is mainly caused by the variability in structures and loa...
International audienceAA2618 aeronautical aluminum alloy has been largely used in the past, especial...
This study deals with the aircraft wing analysis (numerical and experimental) which subjected to fat...
Tensile and fatigue testing results of D357 and B201 aluminum alloy aerospace castings reported in t...
Abstract: The paper presents comparison of three methods of fatigue life assessment related to alumi...
The paper presents comparison of three methods of fatigue life assessment related to aluminium alloy...