The objective of this study is to evaluate the capability of the Impulse Excitation Technique (IET) in assessing the residual elastic properties of damaged composite laminates. To this aim, the Young's modulus in the longitudinal direction of undamaged and damaged thick laminates is evaluated both with the IET and with a tensile test, according to the ASTM standard. The differences between the reference ASTM values and the IET values are then interpreted through a simple mechanical model of the damaged laminate. Potentialities and weaknesses in the application of the IET for the assessment of the residual elastic properties are finally discussed and highlighted in the paper
In the last decades, the use of composite materials for structural components is rapidly increasing....
A major concern affecting the efficient use of composite laminates in aerospace industry is the lack...
9 pages, 13 figures.The damage tolerance of various lay-ups of thin carbon/epoxy laminates (1.6–2.2 ...
The objective of this study is to evaluate the capability of the Impulse Excitation Technique (IET) ...
In this work, an innovative experimental methodology is presented for the assessment of damage sever...
Damage complexity represents one of the main limitations to the diffusion of composite materials in ...
The development of damage tolerance strategies in the design of composite structures constitutes a m...
The detection and evaluation of damage in components made by composite materials is one of the main ...
The detection and evaluation of damage in components made by composite materials is one of the main ...
This paper presents the results of an extensive experimental campaign aimed to examine the effect up...
This paper aims to investigate the ability of ultrasonic and electronic speckle pattern interferomet...
Degradation in mechanical properties (compression, flexural and ILS) of glass epoxy composite lamina...
To detect the presence of damage, many structural health monitoring techniques exploit the nonlinear...
Fiber-reinforced laminated composite materials are widely used in aircraft, modern vehicles and ligh...
This paper concerns the experimental analysis of nonlinear response features of a composite laminat...
In the last decades, the use of composite materials for structural components is rapidly increasing....
A major concern affecting the efficient use of composite laminates in aerospace industry is the lack...
9 pages, 13 figures.The damage tolerance of various lay-ups of thin carbon/epoxy laminates (1.6–2.2 ...
The objective of this study is to evaluate the capability of the Impulse Excitation Technique (IET) ...
In this work, an innovative experimental methodology is presented for the assessment of damage sever...
Damage complexity represents one of the main limitations to the diffusion of composite materials in ...
The development of damage tolerance strategies in the design of composite structures constitutes a m...
The detection and evaluation of damage in components made by composite materials is one of the main ...
The detection and evaluation of damage in components made by composite materials is one of the main ...
This paper presents the results of an extensive experimental campaign aimed to examine the effect up...
This paper aims to investigate the ability of ultrasonic and electronic speckle pattern interferomet...
Degradation in mechanical properties (compression, flexural and ILS) of glass epoxy composite lamina...
To detect the presence of damage, many structural health monitoring techniques exploit the nonlinear...
Fiber-reinforced laminated composite materials are widely used in aircraft, modern vehicles and ligh...
This paper concerns the experimental analysis of nonlinear response features of a composite laminat...
In the last decades, the use of composite materials for structural components is rapidly increasing....
A major concern affecting the efficient use of composite laminates in aerospace industry is the lack...
9 pages, 13 figures.The damage tolerance of various lay-ups of thin carbon/epoxy laminates (1.6–2.2 ...