Add to ORKGThe article deals with 2D test of an airfoil in both plain condition and equipped with the trailing edge Gurney flap. Measurement is carried out by means of PIV method in water channel. 2D velocity fields are presented. Results are briefly discussed.Available from STL Prague, CZ / NTK - National Technical LibrarySIGLECZCzech Republi
Abstract The present investigation assesses the method to extract aerodynamic coefficients and surfa...
The main interest of todays research in fluid mechanics is more and more directed to problems where ...
This paper describes PIV experiments of a synthetic jet array. This part of measurements is an impor...
Abstract: The current paper reviews the research on NACA 23012 and FX66-17AII-182 aerofoils, aerodyn...
The article deals with a Particle Image Velocimetry measurement on a symmetrical wing section. Geome...
The results of flow visualization by means of PIV method on airfoils with spoilers and high-lift fla...
A study of flow in a stationary model of a two-pass internal coolant passage is presented which focu...
Abstract A NACA 0015 airfoil with and without a Gurney flap was studied in a wind tunnel with Rec = ...
In order to acquire experimental data on an airfoil at high angles of attack, wind tunnel tests were...
The Gurney flap is a simple device for increasing the normal force (lift or downforce) generated by ...
The objectives of this stuy were to document mean flow features at high-lift on a mildly swept wing ...
Particle Image Velocimetry (PIV) is increasingly used to investigate unsteady velocity field instant...
The thesis describes the application of particle image velocimetry (PIV) to study the aerodynamic lo...
A two-dimensional numerical investigation was performed to determine the effect of a Gurney flap on ...
The article deals with problems of using of measurement method Particle Image Velocimetry (PIV) to m...
Abstract The present investigation assesses the method to extract aerodynamic coefficients and surfa...
The main interest of todays research in fluid mechanics is more and more directed to problems where ...
This paper describes PIV experiments of a synthetic jet array. This part of measurements is an impor...
Abstract: The current paper reviews the research on NACA 23012 and FX66-17AII-182 aerofoils, aerodyn...
The article deals with a Particle Image Velocimetry measurement on a symmetrical wing section. Geome...
The results of flow visualization by means of PIV method on airfoils with spoilers and high-lift fla...
A study of flow in a stationary model of a two-pass internal coolant passage is presented which focu...
Abstract A NACA 0015 airfoil with and without a Gurney flap was studied in a wind tunnel with Rec = ...
In order to acquire experimental data on an airfoil at high angles of attack, wind tunnel tests were...
The Gurney flap is a simple device for increasing the normal force (lift or downforce) generated by ...
The objectives of this stuy were to document mean flow features at high-lift on a mildly swept wing ...
Particle Image Velocimetry (PIV) is increasingly used to investigate unsteady velocity field instant...
The thesis describes the application of particle image velocimetry (PIV) to study the aerodynamic lo...
A two-dimensional numerical investigation was performed to determine the effect of a Gurney flap on ...
The article deals with problems of using of measurement method Particle Image Velocimetry (PIV) to m...
Abstract The present investigation assesses the method to extract aerodynamic coefficients and surfa...
The main interest of todays research in fluid mechanics is more and more directed to problems where ...
This paper describes PIV experiments of a synthetic jet array. This part of measurements is an impor...