Add to ORKGThere is analysed the use of the acoustical emission (AE) method for non-assembling checking of technical state of complex structures. The control of initiation and development of fatigue cracks by means of different AE systems during fatigue testing of aircraft landing gear component is discussed
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
Acoustic Emission (AE) is a technique for performing Non-Destructive Evaluation (NDE) of structures,...
AbstractAirworthiness regulations require operating advanced aircraft structures in compliance with ...
A technology of early detection and growth control of fatigue damage of vital constructions (for exa...
In the process of fatigue testing it is important to register the arising of the fatigue damages at ...
Aircraft structures fatigue failure is considerable risk of today´s aviation safety. The problem is ...
The acoustic emission (AE) phenomenon has many attributes that make it desirable as a structural hea...
The different kinds of fatigue tests are necessary to continue the life of ageing aircraft. The feat...
In this article it is analyzed possibility of correlation between acoustic emission (AE) parameters ...
Acoustic emission (AE) method is a contemporary and perspective method for aircraft structural assem...
The study is devoted to a perspective diagnostic method, which makes it possible to deal with diagno...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
A shock absorber cylinder of aircraft landing gear leg was used as object of investigation. In proce...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
Acoustic Emission (AE) is a technique for performing Non-Destructive Evaluation (NDE) of structures,...
AbstractAirworthiness regulations require operating advanced aircraft structures in compliance with ...
A technology of early detection and growth control of fatigue damage of vital constructions (for exa...
In the process of fatigue testing it is important to register the arising of the fatigue damages at ...
Aircraft structures fatigue failure is considerable risk of today´s aviation safety. The problem is ...
The acoustic emission (AE) phenomenon has many attributes that make it desirable as a structural hea...
The different kinds of fatigue tests are necessary to continue the life of ageing aircraft. The feat...
In this article it is analyzed possibility of correlation between acoustic emission (AE) parameters ...
Acoustic emission (AE) method is a contemporary and perspective method for aircraft structural assem...
The study is devoted to a perspective diagnostic method, which makes it possible to deal with diagno...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
A shock absorber cylinder of aircraft landing gear leg was used as object of investigation. In proce...
This work forms part of a larger investigation into fatigue crack detection using acoustic emission ...
Acoustic Emission (AE) is a technique for performing Non-Destructive Evaluation (NDE) of structures,...
AbstractAirworthiness regulations require operating advanced aircraft structures in compliance with ...