Add to ORKGPurpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crack growth in aircraft structure. A special AE system was developed and installed on a RAAF Macchi jet trainer. It has been effectively measuring AE from a fatigue crack since August, 1978. Work is continuing to investigate correlation of AE data with crack growth
The purpose of this research was to replicate the fatigue cracking that occurs in aircraft placed un...
Acoustic emission was used for the detection of fatigue cracking in a number of high-strength light ...
Acoustic Emission (AE) is recognized for its potential as a Structural Health Monitoring (SHM) techn...
Purpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crac...
Since the mid-1970s, several studies have investigated the feasibility of using acoustic emission (A...
This paper provides an overview of an ongoing program to utilize acoustic emission methods to detect...
The detection of crack growth in aircraft structures through the use of acoustic emission techniques...
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...
A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying ho...
Acoustic emission (AE) nondestructive testing can detect fatigue cracks as they occur in complex str...
Acoustic emission (AE) is one of several promising non-destructive inspection (NDI) techniques for a...
A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying ho...
AcousQc: emission has emerged as a technique for cletectins crack srowth in a wide ranse of material...
Traditional methods of non-destructive testing (NDT) are used to check the growth of fatigue cracks ...
The purpose of this research was to replicate the fatigue cracking that occurs in aircraft placed un...
Acoustic emission was used for the detection of fatigue cracking in a number of high-strength light ...
Acoustic Emission (AE) is recognized for its potential as a Structural Health Monitoring (SHM) techn...
Purpose of the program is to evaluate acoustic emission (AE) for in-flight detection of fatigue crac...
Since the mid-1970s, several studies have investigated the feasibility of using acoustic emission (A...
This paper provides an overview of an ongoing program to utilize acoustic emission methods to detect...
The detection of crack growth in aircraft structures through the use of acoustic emission techniques...
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...
A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying ho...
Acoustic emission (AE) nondestructive testing can detect fatigue cracks as they occur in complex str...
Acoustic emission (AE) is one of several promising non-destructive inspection (NDI) techniques for a...
A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying ho...
AcousQc: emission has emerged as a technique for cletectins crack srowth in a wide ranse of material...
Traditional methods of non-destructive testing (NDT) are used to check the growth of fatigue cracks ...
The purpose of this research was to replicate the fatigue cracking that occurs in aircraft placed un...
Acoustic emission was used for the detection of fatigue cracking in a number of high-strength light ...
Acoustic Emission (AE) is recognized for its potential as a Structural Health Monitoring (SHM) techn...