This paper presents a novel application of multiparameter spectral theory to the study of structural stability, with particular emphasis on aeroelastic flutter. Methods of multiparameter analysis allow the development of new solution algorithms for aeroelastic flutter problems; most significantly, a direct solver for polynomial problems of arbitrary order and size, something which has not before been achieved. Two major variants of this direct solver are presented, and their computational characteristics are compared. Both are effective for smaller problems arising in reduced-order modelling and preliminary design optimization. Extensions and improvements to this new conceptual framework and solution method are then discussed
In this work an improved mode tracking algorithm is developed for the p-L flutter solution method. C...
AbstractAir vehicles undergo variations in structural mass and stiffness because of fuel consumption...
Free vibration and flutter analyses of two types of high aspect ratio aircraft wings are presented. ...
This paper presents a new method of identifying and analysing stability boundaries in parametric sys...
In this thesis we explore the relationship between aeroelastic flutter and multiparameter spectral t...
This paper presents a novel application of multiparameter spectral theory to the study of structural...
This paper presents several new methods for the solution of aeroelastic flutter problems with a part...
Two analytical flutter solution approaches have been developed to optimize two and three dimensional...
A new method of calculating flutter boundaries of undamped aeronautical structures is presented. The...
peer reviewedDesign against flutter is an important task when designing a flexible structure. Spect...
The stability of linear systems defined by ordinary differential equations with constant or periodic...
An alternative solution to the flutter equation with a true damping representation is presented. The...
The present work describes an alternative methodology for identification of aeroelastic stability in...
This thesis is set out as follows: In Chapter 1, the definition of flutter is given, together with a...
Most of the established procedures for analysis of aeroelastic flutter in the development of aircraf...
In this work an improved mode tracking algorithm is developed for the p-L flutter solution method. C...
AbstractAir vehicles undergo variations in structural mass and stiffness because of fuel consumption...
Free vibration and flutter analyses of two types of high aspect ratio aircraft wings are presented. ...
This paper presents a new method of identifying and analysing stability boundaries in parametric sys...
In this thesis we explore the relationship between aeroelastic flutter and multiparameter spectral t...
This paper presents a novel application of multiparameter spectral theory to the study of structural...
This paper presents several new methods for the solution of aeroelastic flutter problems with a part...
Two analytical flutter solution approaches have been developed to optimize two and three dimensional...
A new method of calculating flutter boundaries of undamped aeronautical structures is presented. The...
peer reviewedDesign against flutter is an important task when designing a flexible structure. Spect...
The stability of linear systems defined by ordinary differential equations with constant or periodic...
An alternative solution to the flutter equation with a true damping representation is presented. The...
The present work describes an alternative methodology for identification of aeroelastic stability in...
This thesis is set out as follows: In Chapter 1, the definition of flutter is given, together with a...
Most of the established procedures for analysis of aeroelastic flutter in the development of aircraf...
In this work an improved mode tracking algorithm is developed for the p-L flutter solution method. C...
AbstractAir vehicles undergo variations in structural mass and stiffness because of fuel consumption...
Free vibration and flutter analyses of two types of high aspect ratio aircraft wings are presented. ...