ABSTRACT: Since thin-walled composite structures are widely used in structural engineer-ing, damage in such structures is an important issue of research. Matrix cracking is a principal cause of failure in composites. In the present study, a composite matrix cracking model is implemented in a thin-walled hollow circular cantilever beam using an effective stiffness approach. Such structures are used to model connecting shafts and helicopter tail boom, for example, because of their high stiffness-to-weight ratios and excellent crashworthiness characteristics. The effect of variation in crack density on the fundamental frequency, for various combinations of m=90ns composite is studied. Using these change in frequencies due to matrix cracking, a...
A structural health monitoring (SHM) methodology is developed for composite rotor blades. An aeroela...
A structural health monitoring (SHM) methodology is developed for composite rotor blades. An aeroela...
Most structural failures are due to break in consisting materials. These breaks begin with a crack, ...
Since thin-walled composite structures are widely used in structural engineering, damage in such str...
Since thin-walled composite structures are widely used in structural engineering, damage in such str...
The suitability of a new fuzzy genetic fused system is investigated in this study for damage identif...
The suitability of a new fuzzy genetic fused system is investigated in this study for damage identif...
Structural damage detection is an inverse problem of structural engineering having three main parts:...
Early detection of damage is of special concern for engineering structures. The traditional methods ...
Early detection of damage is of special concern for engineering structures. The traditional methods ...
Early detection of damage is of special concern for engineering structures. The traditional methods ...
This paper investigates the feasibility of an on-line damage detection capability for helicopter mai...
This paper investigates the feasibility of an on-line damage detection capability for helicopter mai...
This paper presents a novel hybrid fuzzy logic based artificial intelligence (AI) technique applicab...
The method of detecting crack location and its intensity in beam structures by fuzzy logic technique...
A structural health monitoring (SHM) methodology is developed for composite rotor blades. An aeroela...
A structural health monitoring (SHM) methodology is developed for composite rotor blades. An aeroela...
Most structural failures are due to break in consisting materials. These breaks begin with a crack, ...
Since thin-walled composite structures are widely used in structural engineering, damage in such str...
Since thin-walled composite structures are widely used in structural engineering, damage in such str...
The suitability of a new fuzzy genetic fused system is investigated in this study for damage identif...
The suitability of a new fuzzy genetic fused system is investigated in this study for damage identif...
Structural damage detection is an inverse problem of structural engineering having three main parts:...
Early detection of damage is of special concern for engineering structures. The traditional methods ...
Early detection of damage is of special concern for engineering structures. The traditional methods ...
Early detection of damage is of special concern for engineering structures. The traditional methods ...
This paper investigates the feasibility of an on-line damage detection capability for helicopter mai...
This paper investigates the feasibility of an on-line damage detection capability for helicopter mai...
This paper presents a novel hybrid fuzzy logic based artificial intelligence (AI) technique applicab...
The method of detecting crack location and its intensity in beam structures by fuzzy logic technique...
A structural health monitoring (SHM) methodology is developed for composite rotor blades. An aeroela...
A structural health monitoring (SHM) methodology is developed for composite rotor blades. An aeroela...
Most structural failures are due to break in consisting materials. These breaks begin with a crack, ...