Add to ORKGA crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying hours. Acoustic emission data was detected which indicated that during climb, following take-off,the 3mm crack made unstable advances on a few occasions. The detected crack advances produced about 1mm2 of new fracture surface
Traditional methods of non-destructive testing (NDT) are used to check the growth of fatigue cracks ...
AcousQc: emission has emerged as a technique for cletectins crack srowth in a wide ranse of material...
A polyphenylane oxide insulated, flight weight, subscale, aluminum tank was monitored for acoustic e...
A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying ho...
The relation of the occurrence of airframe acoustic emissions to aircraft manoeuvre are reported for...
The detection of crack growth in aircraft structures through the use of acoustic emission techniques...
Since the mid-1970s, several studies have investigated the feasibility of using acoustic emission (A...
Purpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crac...
Purpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crac...
Since the mid-1970’s several authors have investigated the feasibility of using acoustic emission to...
During the past 20 years acoustic emission has been applied successfully to numerous materials degra...
This paper provides an overview of an ongoing program to utilize acoustic emission methods to detect...
Acoustic emission (AE) is one of several promising non-destructive inspection (NDI) techniques for a...
Acoustic emission (AE) nondestructive testing can detect fatigue cracks as they occur in complex str...
During the past 20 years acoustic emission has been applied successfully to numerous materials degra...
Traditional methods of non-destructive testing (NDT) are used to check the growth of fatigue cracks ...
AcousQc: emission has emerged as a technique for cletectins crack srowth in a wide ranse of material...
A polyphenylane oxide insulated, flight weight, subscale, aluminum tank was monitored for acoustic e...
A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying ho...
The relation of the occurrence of airframe acoustic emissions to aircraft manoeuvre are reported for...
The detection of crack growth in aircraft structures through the use of acoustic emission techniques...
Since the mid-1970s, several studies have investigated the feasibility of using acoustic emission (A...
Purpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crac...
Purpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crac...
Since the mid-1970’s several authors have investigated the feasibility of using acoustic emission to...
During the past 20 years acoustic emission has been applied successfully to numerous materials degra...
This paper provides an overview of an ongoing program to utilize acoustic emission methods to detect...
Acoustic emission (AE) is one of several promising non-destructive inspection (NDI) techniques for a...
Acoustic emission (AE) nondestructive testing can detect fatigue cracks as they occur in complex str...
During the past 20 years acoustic emission has been applied successfully to numerous materials degra...
Traditional methods of non-destructive testing (NDT) are used to check the growth of fatigue cracks ...
AcousQc: emission has emerged as a technique for cletectins crack srowth in a wide ranse of material...
A polyphenylane oxide insulated, flight weight, subscale, aluminum tank was monitored for acoustic e...