1 Introduction 2 1.1 Flow Regimes . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 1.2 Goals & Outline . . . . . . . . . . . . . . . . . . . . . . . . . . 6 2 Geometry and Numerical Methodology 7 2.1 Geometry and Numerical Set-up . . . . . . . . . . . . . . . . . 7 2.2 Numerical Model . . . . . . . . . . . . . . . . . . . . . . . . . 10 2.3 Post-Processing . . . . . . . . . . . . . . . . . . . . . . . . . . 11 3 Mesh and First Results 12 3.1 Mesh Sensitivity Analysis . . . . . . . . . . . . . . . . . . . . 12 3.2 Results: Re = 300 . . . . . . . . . . . . . . . . . . . . . . . . . 15 3.3 Results: Re = 800 . . . . . . . . . . . . . . . . . . . . . . . . . 19 3.4 Results: Re = 1500 . . . . . . . . . . . . . . . . . . . . . . . . 19 4 In...
A computer program has been developed to calculate laminar layers along inviscid surface streamlines...
The flow around a vehicle, for example, results in a large resistance and can generate a complex swi...
As part of an effort to develop computational techniques for design of natural laminar flow fuselage...
The influence of the thickness of the boundary layer developing over the surface of an axisymmetric ...
This work is a part of an experimental and numerical research activity aimed at characterizing and r...
A wind tunnel investigation is carried out to study the influence of the characteristics of the boun...
In this work the results are described of a wind tunnel investigation carried out to study the influ...
The variation of the base drag of an axisymmetric bluff body caused by modifications of the boundary...
In the present work, the main findings of an experimental and numerical research activity aimed at c...
Boundary layer on the cylindrical portion of an\ud Axisymmetric underwater body is measured at three...
This thesis studies the effect of turbulent boundary layer thickness on the wake dynamics of a blunt...
This paper presents the effect of axisymmetric forebody shapes on the global stability characteristi...
The aim of this work is to analyze a viscous flow around the axisymmetric blunt body taken into acco...
ABSTRACT: This research project focuses upon the wake behind a two-dimensional blunt-trailing-edged ...
The wake behind a rectangular forebody with variable inlet conditions is investigated. The perforate...
A computer program has been developed to calculate laminar layers along inviscid surface streamlines...
The flow around a vehicle, for example, results in a large resistance and can generate a complex swi...
As part of an effort to develop computational techniques for design of natural laminar flow fuselage...
The influence of the thickness of the boundary layer developing over the surface of an axisymmetric ...
This work is a part of an experimental and numerical research activity aimed at characterizing and r...
A wind tunnel investigation is carried out to study the influence of the characteristics of the boun...
In this work the results are described of a wind tunnel investigation carried out to study the influ...
The variation of the base drag of an axisymmetric bluff body caused by modifications of the boundary...
In the present work, the main findings of an experimental and numerical research activity aimed at c...
Boundary layer on the cylindrical portion of an\ud Axisymmetric underwater body is measured at three...
This thesis studies the effect of turbulent boundary layer thickness on the wake dynamics of a blunt...
This paper presents the effect of axisymmetric forebody shapes on the global stability characteristi...
The aim of this work is to analyze a viscous flow around the axisymmetric blunt body taken into acco...
ABSTRACT: This research project focuses upon the wake behind a two-dimensional blunt-trailing-edged ...
The wake behind a rectangular forebody with variable inlet conditions is investigated. The perforate...
A computer program has been developed to calculate laminar layers along inviscid surface streamlines...
The flow around a vehicle, for example, results in a large resistance and can generate a complex swi...
As part of an effort to develop computational techniques for design of natural laminar flow fuselage...