Add to ORKGA study has been made on the influence of the leading edge imperfections in airfoils used in different devices relating their aerodynamic performances. Wind tunnel tests have been made at different Reynolds numbers and angle of attacks in order to show this effect. Later, a quantitative study of the aerodynamic properties has been made based on the different leading edge imperfections and their size
These tests show that small changes in airfoil contours, resulting from variations in the specified ...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
This paper presents wind tunnel experiment on two delta wing configurations which are differentiated...
A study has been made on the influence of the leading edge imperfections in airfoils used in differe...
The interest of this study is based on the observation that some manufacturing processes of various...
This article deals with the effect of leading edge imperfections on the aerodynamic characteristics ...
A study has been made on the influence of the open trailing edge in airfoils used in different devic...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
The effect on airfoil characteristics of surface roughness of varying degrees and types at different...
Unexpected performance degradation occurs in wind turbine blades due to leading edge defect when suf...
Low-speed wind-tunnel tests were conducted to determine the two-dimensional aerodynamic characterist...
In this study, the aerodynamic performance of a thick airfoil is analysed, after installing leading-...
Aerodynamic analysis of a low Reynolds number airfoil is critical for numerous applications in the f...
Taking the S823 airfoil as the research object, this study investigates the influence of different t...
abstract: The purpose of this paper is to discover what geometric characteristics of a wing and airf...
These tests show that small changes in airfoil contours, resulting from variations in the specified ...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
This paper presents wind tunnel experiment on two delta wing configurations which are differentiated...
A study has been made on the influence of the leading edge imperfections in airfoils used in differe...
The interest of this study is based on the observation that some manufacturing processes of various...
This article deals with the effect of leading edge imperfections on the aerodynamic characteristics ...
A study has been made on the influence of the open trailing edge in airfoils used in different devic...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
The effect on airfoil characteristics of surface roughness of varying degrees and types at different...
Unexpected performance degradation occurs in wind turbine blades due to leading edge defect when suf...
Low-speed wind-tunnel tests were conducted to determine the two-dimensional aerodynamic characterist...
In this study, the aerodynamic performance of a thick airfoil is analysed, after installing leading-...
Aerodynamic analysis of a low Reynolds number airfoil is critical for numerous applications in the f...
Taking the S823 airfoil as the research object, this study investigates the influence of different t...
abstract: The purpose of this paper is to discover what geometric characteristics of a wing and airf...
These tests show that small changes in airfoil contours, resulting from variations in the specified ...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
This paper presents wind tunnel experiment on two delta wing configurations which are differentiated...