An analytical approach is followed to model unsteady two-dimensional flow fields in multiply connected domains. The inviscid model developed here, capable of determining unsteady flows, is applied to investigate the instantaneous start of biplane configurations, including both unstaggered and tandem arrangements, and a rod-aerofoil system. Following recent advancements of two-dimensional flow modelling via conformal mapping of multiply connected domains, the so-called Schottky-Klein prime function is employed; it is the key function to construct complex potentials associated with multiple objects in the presence of free stream and vortices. In order to generate the complex potential associated with moving objects in a doubly connected domai...
On étudie des phénomènes de séparation d'écoulement avec deux approches différentes. Dans la premièr...
A model for simulating the incompressible flow over a practical airfoil executing a pitching motion ...
The new boundary integral formulation for the velocity field in Aerodynamics, proposed in Part I, is...
Inviscid analytical-numerical model for predicting unsteady forces on two aerofoil configurations is...
This book builds inviscid flow analysis from an undergraduate-level treatment of potential flow to t...
In the present work flow separation phenomena are investigated by means of two different approaches....
A potential flow model is used to study the unsteady flow past two airfoils in configuration, each o...
Presented in this report is a new method for the prediction of unsteady, incompressible separated fl...
Steady and unsteady flowfields around an airfoil are simulated numerically using a compressible Navi...
{Steady incompressible inviscid flow past a three-dimensional multiconnected (toroidal) aerofoil wit...
Summary: A new model is presented for the calculation of the incompressible, inviscid flow aroun...
Abstract: As well known the solution of the incompressible flow problem in a double-connec...
This paper presents recent advances in a computing method for unsteady inviscid incompressible flows...
The main objectives of this thesis are to implement the one- and two-way couplings of an inviscid fl...
An exact treatment of the problem of finding the incompressible, inviscid two-dimensional flow aroun...
On étudie des phénomènes de séparation d'écoulement avec deux approches différentes. Dans la premièr...
A model for simulating the incompressible flow over a practical airfoil executing a pitching motion ...
The new boundary integral formulation for the velocity field in Aerodynamics, proposed in Part I, is...
Inviscid analytical-numerical model for predicting unsteady forces on two aerofoil configurations is...
This book builds inviscid flow analysis from an undergraduate-level treatment of potential flow to t...
In the present work flow separation phenomena are investigated by means of two different approaches....
A potential flow model is used to study the unsteady flow past two airfoils in configuration, each o...
Presented in this report is a new method for the prediction of unsteady, incompressible separated fl...
Steady and unsteady flowfields around an airfoil are simulated numerically using a compressible Navi...
{Steady incompressible inviscid flow past a three-dimensional multiconnected (toroidal) aerofoil wit...
Summary: A new model is presented for the calculation of the incompressible, inviscid flow aroun...
Abstract: As well known the solution of the incompressible flow problem in a double-connec...
This paper presents recent advances in a computing method for unsteady inviscid incompressible flows...
The main objectives of this thesis are to implement the one- and two-way couplings of an inviscid fl...
An exact treatment of the problem of finding the incompressible, inviscid two-dimensional flow aroun...
On étudie des phénomènes de séparation d'écoulement avec deux approches différentes. Dans la premièr...
A model for simulating the incompressible flow over a practical airfoil executing a pitching motion ...
The new boundary integral formulation for the velocity field in Aerodynamics, proposed in Part I, is...