This article discusses the use of generalized eigenanalysis to extract reduced order models from the linearization of structural and aeroelastic problems written in differential-algebraic form. These problems may arise from multi-body analysis and in general from mixed approaches, where a high degree of generality and modelling flexibility are sought. A method based on a shift technique is proposed, that allows to exploit the regularity of the matrix pencil resulting from the linearization of differential-algebraic problems. Alternatively, the generalized Schur decomposition, or QZ decomposition, is directly used to select a cluster of eigenvalues related to the dynamic states. The two approaches are used to reduce the model to ordinary dif...
This paper presents a methodology for the identification of a reduced-order model (ROM) for the pert...
A nonlinear model reduction based on eigenmode decomposition and projection for the prediction of su...
An alternative solution to the flutter equation with a true damping representation is presented. The...
This article discusses the use of generalized eigenanalysis to extract reduced order models from the...
The stability of linear systems defined by ordinary differential equations with constant or periodic...
Physical structures and processes are modeled by dynamical systems in a wide range of application ar...
A procedure for approximating the aerodynamic matrix as a reduced order model is introduced. This al...
General methodology for calculating changes in eigenvalues and eigenvectors resulting from parameter...
The Generalized Aeroelastic Analysis Method (GAAM) is applied to the analysis of three well-studied ...
Design of modern control laws motivates the creation of state-space models from aeroservoelastic mod...
International audienceThis paper deals with the extension of proper generalized decomposition method...
In this paper, we review the development of new reduced-order modeling techniques and discuss their ...
Time domain aeroelastic analysis has high computing costs when using computational fluid dynamics. T...
This paper deals with the extension of Proper Generalized Decomposition (PGD) methods to non-linear ...
Three types of aeroelastic reduced-order models (ROMs) for flutter and gust-response analyses are ex...
This paper presents a methodology for the identification of a reduced-order model (ROM) for the pert...
A nonlinear model reduction based on eigenmode decomposition and projection for the prediction of su...
An alternative solution to the flutter equation with a true damping representation is presented. The...
This article discusses the use of generalized eigenanalysis to extract reduced order models from the...
The stability of linear systems defined by ordinary differential equations with constant or periodic...
Physical structures and processes are modeled by dynamical systems in a wide range of application ar...
A procedure for approximating the aerodynamic matrix as a reduced order model is introduced. This al...
General methodology for calculating changes in eigenvalues and eigenvectors resulting from parameter...
The Generalized Aeroelastic Analysis Method (GAAM) is applied to the analysis of three well-studied ...
Design of modern control laws motivates the creation of state-space models from aeroservoelastic mod...
International audienceThis paper deals with the extension of proper generalized decomposition method...
In this paper, we review the development of new reduced-order modeling techniques and discuss their ...
Time domain aeroelastic analysis has high computing costs when using computational fluid dynamics. T...
This paper deals with the extension of Proper Generalized Decomposition (PGD) methods to non-linear ...
Three types of aeroelastic reduced-order models (ROMs) for flutter and gust-response analyses are ex...
This paper presents a methodology for the identification of a reduced-order model (ROM) for the pert...
A nonlinear model reduction based on eigenmode decomposition and projection for the prediction of su...
An alternative solution to the flutter equation with a true damping representation is presented. The...