Two reduction methods for dynamic analysis of structures with local nonlinearity are compared. Dual and primal formulation have the same projection basis including flexibility residual attachment modes and free interface modes, but there are significant differences in their implementation. Both methods can be applied to nonlinear forced response analysis of turbine blades with contact interfaces in shroud. In this study, the shroud contact elements are employed using the adequate description of friction and 3D tangential coupled contact forces considering the effect of normal load variation. In order to examine and compare the accuracy of the two formulations, a rod and a simplified shrouded turbine blade was considered as case studie...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
High-cycle fatigue is one of the most frequent reasons of failure for turbomachinery and in early de...
Aim of this research is the prediction of the non-linear forced response of a stator bladed disk for...
The efficient dynamic stress assessment of turbine blades is of prime importance in turbomachinery d...
A highly accurate and computationally efficient method is proposed for reduced modeling of jointed s...
peer reviewedThis paper investigates the use of different model reduction methods accounting for geo...
Actual trend in steam turbine design is to use blades with integral shrouds, for high pressure and i...
This thesis examines the forced, non-linear vibration of integral shroud turbine blades. The shroud ...
A coupled static-dynamic method is proposed and applied to bladed disks with shrouds, in order to ca...
peer reviewedThis paper deals with the reduced order modeling of turbomachine bladed structures acco...
peer reviewedThis article presents a methodology dedicated to the vibration analysis of turbomachine...
In this paper, a forced response prediction method for the analysis of constrained and unconstrained...
An effective method has been developed to calculate the sensitivity of the resonance peak frequency ...
The prediction of the aeromechanical behavior of low-pressure blades represents one of the main chal...
An analytical expression is formulated to compute the Jacobian matrix for 3D friction contact modeli...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
High-cycle fatigue is one of the most frequent reasons of failure for turbomachinery and in early de...
Aim of this research is the prediction of the non-linear forced response of a stator bladed disk for...
The efficient dynamic stress assessment of turbine blades is of prime importance in turbomachinery d...
A highly accurate and computationally efficient method is proposed for reduced modeling of jointed s...
peer reviewedThis paper investigates the use of different model reduction methods accounting for geo...
Actual trend in steam turbine design is to use blades with integral shrouds, for high pressure and i...
This thesis examines the forced, non-linear vibration of integral shroud turbine blades. The shroud ...
A coupled static-dynamic method is proposed and applied to bladed disks with shrouds, in order to ca...
peer reviewedThis paper deals with the reduced order modeling of turbomachine bladed structures acco...
peer reviewedThis article presents a methodology dedicated to the vibration analysis of turbomachine...
In this paper, a forced response prediction method for the analysis of constrained and unconstrained...
An effective method has been developed to calculate the sensitivity of the resonance peak frequency ...
The prediction of the aeromechanical behavior of low-pressure blades represents one of the main chal...
An analytical expression is formulated to compute the Jacobian matrix for 3D friction contact modeli...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
High-cycle fatigue is one of the most frequent reasons of failure for turbomachinery and in early de...
Aim of this research is the prediction of the non-linear forced response of a stator bladed disk for...