Add to ORKGThe phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was investigated at cyclic loading. Mentioned effect is associated with the crack open/close that change acoustic impedance of a crack. Analytical simulation of fatigue crack opening using the generalized Dugdale’s model of a crack in thin plate shows good accordance between the intensity of ultrasonic signal and a crack opening. The perspective of application for structural health monitoring (SHM) of aircraf
This article is connected with 6FP Euro project AISHA. The basic purpose of the project is developme...
In this paper, we investigated transducer placement strategies for detecting cracks in primary aircr...
The paper presents a method for detection mechanisms and prevention of the fatigue cracks caused by ...
The phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was investigated a...
The phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was in-vestigated ...
The phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was investigated a...
The establishment of reliable correlations between the extend of damage and a sensor response using...
Structural health monitoring of riveted aircraft panels is a real challenge for maintenance engineer...
The establishment of reliable correlations between parameters of damage and a sensor response during...
The establishment of reliable correlations between parameters of damage and a sensor response during...
Investigation of ultrasonic Lamb wave interaction with a fatigue crack has been executed on flat sa...
Structural health monitoring has focused on the use of computational models to capture the effect of...
The development of fatigue cracks at fastener holes represents a common maintenance problem for airc...
Especially for ageing aircraft the development of fatigue cracks at fastener holes due to stress con...
The reliability of fatigue-crack detection plays an important role in the safety of aircraft structu...
This article is connected with 6FP Euro project AISHA. The basic purpose of the project is developme...
In this paper, we investigated transducer placement strategies for detecting cracks in primary aircr...
The paper presents a method for detection mechanisms and prevention of the fatigue cracks caused by ...
The phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was investigated a...
The phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was in-vestigated ...
The phenomenon of the Lamb wave interaction with fatigue crack in Al2024-T3 sheet was investigated a...
The establishment of reliable correlations between the extend of damage and a sensor response using...
Structural health monitoring of riveted aircraft panels is a real challenge for maintenance engineer...
The establishment of reliable correlations between parameters of damage and a sensor response during...
The establishment of reliable correlations between parameters of damage and a sensor response during...
Investigation of ultrasonic Lamb wave interaction with a fatigue crack has been executed on flat sa...
Structural health monitoring has focused on the use of computational models to capture the effect of...
The development of fatigue cracks at fastener holes represents a common maintenance problem for airc...
Especially for ageing aircraft the development of fatigue cracks at fastener holes due to stress con...
The reliability of fatigue-crack detection plays an important role in the safety of aircraft structu...
This article is connected with 6FP Euro project AISHA. The basic purpose of the project is developme...
In this paper, we investigated transducer placement strategies for detecting cracks in primary aircr...
The paper presents a method for detection mechanisms and prevention of the fatigue cracks caused by ...