Based on the dependence of fatigue crack growth( FCG) threshold on stress ratio,a low-load-truncation method for FCG tests is proposed. The effects of FCG property,stress amplitude and stress ratio are considered by this method. FCG tests using middle tension( M( T)) specimens under a flight-by-flight spectrum and two truncated spectra were conducted. The difference between FCG lives under truncated spectra and those under baseline spectrum is less than 26%,but the test duration were shorten by 78% maximum. The test results indicate that the proposed low-load-truncation method can shorten FCG test period effectively without changing the failure mode or changing the FCG life irrationally
Whilst crack growth retardation following the application of an overload during variable amplitude l...
Many aircraft are designed using the Damage-Tolerance concept. This concept assumes that a structura...
Military aircraft are subjected to variable loads, which are the main cause of initiation and propag...
AbstractTests with middle-crack tension (M(T)) specimens made of Al 2324-T39 and Al 7050-T7451 are c...
A new subsection-loading method has been used for solving question that was taken for aircraft struc...
ABSTRACT: Constant amplitude fatigue crack growth (FCG) tests were performed at various stress ratio...
ABSTRACT: Constant amplitude fatigue crack growth (FCG) tests were performed at various stress ratio...
The flight load sequence of a combat aircraft was modified by eliminating different levels of small ...
The definition of the load spectrum of the full-scale fatigue test of a new aircraft is a very delic...
AbstractThe paper summarizes conclusions based on fatigue crack growth experiments and numerical cal...
In order to accelerate full scale fatigue testing, the original flight load spectrum of a combat air...
This project involved development of a method to predict the fatigue crack propagation process in th...
The damage tolerance concept is widely used in the aircraft industry to analyze the fatigue life of ...
The fatigue or durability life of a few critical structural metallic components often sets the safe ...
Fatigue is a well-recognized issue in lightweight and high-performance aircraft structures. As fatig...
Whilst crack growth retardation following the application of an overload during variable amplitude l...
Many aircraft are designed using the Damage-Tolerance concept. This concept assumes that a structura...
Military aircraft are subjected to variable loads, which are the main cause of initiation and propag...
AbstractTests with middle-crack tension (M(T)) specimens made of Al 2324-T39 and Al 7050-T7451 are c...
A new subsection-loading method has been used for solving question that was taken for aircraft struc...
ABSTRACT: Constant amplitude fatigue crack growth (FCG) tests were performed at various stress ratio...
ABSTRACT: Constant amplitude fatigue crack growth (FCG) tests were performed at various stress ratio...
The flight load sequence of a combat aircraft was modified by eliminating different levels of small ...
The definition of the load spectrum of the full-scale fatigue test of a new aircraft is a very delic...
AbstractThe paper summarizes conclusions based on fatigue crack growth experiments and numerical cal...
In order to accelerate full scale fatigue testing, the original flight load spectrum of a combat air...
This project involved development of a method to predict the fatigue crack propagation process in th...
The damage tolerance concept is widely used in the aircraft industry to analyze the fatigue life of ...
The fatigue or durability life of a few critical structural metallic components often sets the safe ...
Fatigue is a well-recognized issue in lightweight and high-performance aircraft structures. As fatig...
Whilst crack growth retardation following the application of an overload during variable amplitude l...
Many aircraft are designed using the Damage-Tolerance concept. This concept assumes that a structura...
Military aircraft are subjected to variable loads, which are the main cause of initiation and propag...