Wind tunnel tests of a laminar airfoil have been performed at the Institute of Aviation in
Warsaw. The main goal of the investigation was to study the separation process …

Study of transition location effect (from natural transition to fully turbulent) on separation size,
shock structure and unsteadiness was the focus of this WP. Boundary layer tripping (by wire …

The wind tunnel investigation of basic aerodynamic characteristics as well as flow
visualization tests of the innovative quad-rotor autogyro model is presented. The wind tunnel …

Purpose The simulations of grid-resolved rod vortex generators (RVGs) require high
computational cost and time. Additionally, the computational mesh topology must be …

The evolution of artificial disturbances in a laminar boundary layer on a flat plate model in
the presence of an incident shock wave is considered. The flow is supersonic with the …

The paper deals with study the area of interaction incident shock wave with a laminar
boundary layer by PIV technique. The several data processing techniques to determine PIV …

An experimental study of the zone of a shock wave with a boundary layer interaction,
developing on a flat plate is carried out. The laminar as major and turbulent as addition …

W pracy przedstawiono analizę możliwości wykorzystania metody elementów skończonych
do określenia wpływu rozpraszaczy wirów brzegowych (ang. winglet) na charakterystyki …