Sandwich structures are very attractive due to their high strength at a minimum weight, and, therefore, there has been a rapid increase in their applications. Nevertheless, these structures may present imperfect bonding or debonding between the skins and core as a result of manufacturing defects or impact loads, degrading their mechanical properties. To improve both the safety and functionality of these systems, structural damage assessment methodologies can be implemented. This article presents a damage assessment algorithm to localize and quantify debonds in sandwich panels. The proposed algorithm uses damage indices derived from the modal strain energy method and a linear approximation with a maximum entropy algorithm. Full-field vibrati...
Artículo de publicación ISIHoneycomb sandwich structures are used in a wide variety of applications....
А survey of recent developments in the dynamic analysis of sandwich panels with face sheet-to-core ...
Structural Health Monitoring (SHM) techniques are emerging more and more in aerospace composite stru...
Sandwich structures are very attractive due to their high strength at a minimum weight, and, therefo...
Different studies have demonstrated that vibration characteristics are sensitive to debonding in com...
Different studies have demonstrated that vibration characteristics are sensitive to debonding in co...
Honeycomb sandwich structures are used in a wide variety of applications. Nevertheless, due to manuf...
The vibrational behavior of composite structures has been demonstrated as a useful feature for ident...
A survey of recent developments in the dynamic analysis of sandwich panels with face sheet-to-core d...
The possibility of using a new diagnostic technique to identify the presence of localised debonding ...
A vibration-based non-destructive evaluation (NDE) method is proposed to determine the location and ...
A damage-identification method based on flexibility matrix and Teager energy operator is proposed fo...
A sandwich construction is a special form of the laminated composite consisting of light weight core...
A vibration-based damage identification method, based on changes in modal strain energies before and...
Previously, an evaluation study has been conducted on a Structural Health Monitoring (SHM) strategy ...
Artículo de publicación ISIHoneycomb sandwich structures are used in a wide variety of applications....
А survey of recent developments in the dynamic analysis of sandwich panels with face sheet-to-core ...
Structural Health Monitoring (SHM) techniques are emerging more and more in aerospace composite stru...
Sandwich structures are very attractive due to their high strength at a minimum weight, and, therefo...
Different studies have demonstrated that vibration characteristics are sensitive to debonding in com...
Different studies have demonstrated that vibration characteristics are sensitive to debonding in co...
Honeycomb sandwich structures are used in a wide variety of applications. Nevertheless, due to manuf...
The vibrational behavior of composite structures has been demonstrated as a useful feature for ident...
A survey of recent developments in the dynamic analysis of sandwich panels with face sheet-to-core d...
The possibility of using a new diagnostic technique to identify the presence of localised debonding ...
A vibration-based non-destructive evaluation (NDE) method is proposed to determine the location and ...
A damage-identification method based on flexibility matrix and Teager energy operator is proposed fo...
A sandwich construction is a special form of the laminated composite consisting of light weight core...
A vibration-based damage identification method, based on changes in modal strain energies before and...
Previously, an evaluation study has been conducted on a Structural Health Monitoring (SHM) strategy ...
Artículo de publicación ISIHoneycomb sandwich structures are used in a wide variety of applications....
А survey of recent developments in the dynamic analysis of sandwich panels with face sheet-to-core ...
Structural Health Monitoring (SHM) techniques are emerging more and more in aerospace composite stru...