A modeling method for the modal analysis of a multi-blade system undergoing rotational motion is presented in this paper. Blades are assumed as cantilever beams and the coupling stiffness which originates from the shroud flexibility is considered for the modeling. To obtain general conclusions from the numerical results, the equations of motion are transformed into a dimensionless form. Dimensionless parameters related to the angular speed, the hub radius, and the coupling stiffness are identified and the effects of the parameters on the modal characteristics of the system are investigated. It is shown that the coupling stiffness especially plays an important role to change the modal characteristics of the system. The range of critical angu...
During fast gas-turbine engine acceleration and deceleration the transient vibration effects in blad...
The process of structural dynamic modelling of the flexible rotor blade in a multibody system is dem...
In this paper, we propose a new nonlinear dynamic model of a rotor-blade system with whirling motion...
A modeling method for the modal analysis of a multi-packet blade system undergoing rotational motion...
A modeling method for the modal analysis of a multi-packet blade system undergoing rotational motion...
Free vibration analysis of a twisted, double-tapered blade mounted on a rotating disk undergoing ove...
A linear geometrical stiffening model is developed for a rotating beam with an asymmetric cross sect...
In this paper the vibrational behavior of a multi-packet blade system having a cracked blade is inve...
The influence of shaft bending on the coupling vibration of rotor-blades system is nonignorable. The...
A geometrically exact mechanical model for the overall dynamics of elastic isotropic rotating blades...
The physics lying behind rotordynamics is complex to model, so that in many cases numerical processi...
International audienceIn modern turbo machines such as aircraft jet engines, contact between the cas...
The vibrations of a rotating blade are strongly influenced by the axial forces that are induced by c...
This paper presents a linear semi-analytical model that is able to predict complex rotor-structure c...
The rotor-bladed systems are commonly used in industrial applications, such as in turbines, ventila...
During fast gas-turbine engine acceleration and deceleration the transient vibration effects in blad...
The process of structural dynamic modelling of the flexible rotor blade in a multibody system is dem...
In this paper, we propose a new nonlinear dynamic model of a rotor-blade system with whirling motion...
A modeling method for the modal analysis of a multi-packet blade system undergoing rotational motion...
A modeling method for the modal analysis of a multi-packet blade system undergoing rotational motion...
Free vibration analysis of a twisted, double-tapered blade mounted on a rotating disk undergoing ove...
A linear geometrical stiffening model is developed for a rotating beam with an asymmetric cross sect...
In this paper the vibrational behavior of a multi-packet blade system having a cracked blade is inve...
The influence of shaft bending on the coupling vibration of rotor-blades system is nonignorable. The...
A geometrically exact mechanical model for the overall dynamics of elastic isotropic rotating blades...
The physics lying behind rotordynamics is complex to model, so that in many cases numerical processi...
International audienceIn modern turbo machines such as aircraft jet engines, contact between the cas...
The vibrations of a rotating blade are strongly influenced by the axial forces that are induced by c...
This paper presents a linear semi-analytical model that is able to predict complex rotor-structure c...
The rotor-bladed systems are commonly used in industrial applications, such as in turbines, ventila...
During fast gas-turbine engine acceleration and deceleration the transient vibration effects in blad...
The process of structural dynamic modelling of the flexible rotor blade in a multibody system is dem...
In this paper, we propose a new nonlinear dynamic model of a rotor-blade system with whirling motion...