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
This paper presents the preliminary results on the aeroacoustic and aerodynamic performances of a NA...
It is well known that roughness effect is detrimental for the aerodynamics performance of a surface ...
Wind tunnel experiments were conducted in order to investigate the effectiveness of flow control dev...
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...
Wind tunnel tests were conducted to examine various aspects of the drooped-leading edge airfoil whic...
Unexpected performance degradation occurs in wind turbine blades due to leading edge defect when suf...
The effect on airfoil characteristics of surface roughness of varying degrees and types at different...
The effect on airfoil characteristics of surface roughness of varying degrees and types at different...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
An investigation was conducted to determine the flow field and aerodynamic effects of leading-edge s...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
The present work has as main objective the experimental analysis of the air flow around a convention...
This paper presents the preliminary results on the aeroacoustic and aerodynamic performances of a NA...
It is well known that roughness effect is detrimental for the aerodynamics performance of a surface ...
Wind tunnel experiments were conducted in order to investigate the effectiveness of flow control dev...
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...
Wind tunnel tests were conducted to examine various aspects of the drooped-leading edge airfoil whic...
Unexpected performance degradation occurs in wind turbine blades due to leading edge defect when suf...
The effect on airfoil characteristics of surface roughness of varying degrees and types at different...
The effect on airfoil characteristics of surface roughness of varying degrees and types at different...
Abstract The NACA 633‐418 airfoil has been tested in the new Poul la Cour Wind Tunnel at the Technic...
An investigation was conducted to determine the flow field and aerodynamic effects of leading-edge s...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
The present work has as main objective the experimental analysis of the air flow around a convention...
This paper presents the preliminary results on the aeroacoustic and aerodynamic performances of a NA...
It is well known that roughness effect is detrimental for the aerodynamics performance of a surface ...
Wind tunnel experiments were conducted in order to investigate the effectiveness of flow control dev...