Optical fractography was used to estimate small notch13; crack growth under programmed FALSTAFF loading in an13; Al-Cu alloy. It was able to handle crack sizes as low as 25 microns and growth rates Over two orders of magnitude. 13; Randomized Mini FALSTAFF load sequence was modified13; into a programmed load equivalent with major loads either13; preceeded or succeeded by marker loads. Crack growth rate13; under programmed FALSTAFF spectrum as estimated by optical13; fractography conformed to compliance based estimates on a13; SE (T) specimen. Long crack growth rates under programmed13; and randomized mini FALSTAFF spectrum were essentially13; similar. Spectrum load fatigue crack growth was studied13; in central hole coupons under notch inel...
A fractographic study was performed on Al-alloy fatigue fracture surfaces produced by programmed loa...
Fatigue crack growth tests were conducted on compact, C(T), specimens made of 7249-T76511 aluminium ...
The fatigue behaviour of aerospace structural components is dominated by the time to grow from a sma...
Optical fractography was used to estimate small notch13; crack growth under programmed FALSTAFF load...
Optical fractography was used to estimate growth of small cracks at notches under programmed FALSTAF...
Optical fractography was used to estimate growth of small cracks at notches under programmed FALSTAF...
The paper describes an experimental study of notch root fatigue crack growth under FALSTAFF spectrum...
The kinetics of short cracks at notches were studied in 2014-T6511 Al-Cu alloy extruded bar stock un...
The kinetics of short cracks at notches were studied in 2014-T6511 Al-Cu alloy extruded bar stock un...
This paper presents an assessment on fatigue crack propagation (FCG) behavior and fractography obser...
Whilst crack growth retardation following the application of an overload during variable amplitude l...
Fatigue crack growth behavior of through-the-thickness cracks emanating from the notch root in an al...
Fatigue crack growth behavior of through-the-thickness cracks emanating from the notch root in an al...
The fatigue or durability life of a few critical structural metallic components often sets the safe ...
Fatigue crack propagation has been observed for a number of commercial aluminium alloys. Comparable ...
A fractographic study was performed on Al-alloy fatigue fracture surfaces produced by programmed loa...
Fatigue crack growth tests were conducted on compact, C(T), specimens made of 7249-T76511 aluminium ...
The fatigue behaviour of aerospace structural components is dominated by the time to grow from a sma...
Optical fractography was used to estimate small notch13; crack growth under programmed FALSTAFF load...
Optical fractography was used to estimate growth of small cracks at notches under programmed FALSTAF...
Optical fractography was used to estimate growth of small cracks at notches under programmed FALSTAF...
The paper describes an experimental study of notch root fatigue crack growth under FALSTAFF spectrum...
The kinetics of short cracks at notches were studied in 2014-T6511 Al-Cu alloy extruded bar stock un...
The kinetics of short cracks at notches were studied in 2014-T6511 Al-Cu alloy extruded bar stock un...
This paper presents an assessment on fatigue crack propagation (FCG) behavior and fractography obser...
Whilst crack growth retardation following the application of an overload during variable amplitude l...
Fatigue crack growth behavior of through-the-thickness cracks emanating from the notch root in an al...
Fatigue crack growth behavior of through-the-thickness cracks emanating from the notch root in an al...
The fatigue or durability life of a few critical structural metallic components often sets the safe ...
Fatigue crack propagation has been observed for a number of commercial aluminium alloys. Comparable ...
A fractographic study was performed on Al-alloy fatigue fracture surfaces produced by programmed loa...
Fatigue crack growth tests were conducted on compact, C(T), specimens made of 7249-T76511 aluminium ...
The fatigue behaviour of aerospace structural components is dominated by the time to grow from a sma...