The advancement of flow measurement techniques continues to extend experimental boundaries and thus significantly contributes to improving our understanding of both basic and applied aerodynamics. This is particularly apparent in the case of particle image velocimetry (PIV), where its application has furthered the existing knowledge in several areas of helicopter rotor aerodynamics. The complex nature of helicopter rotor flows presents unique challenges to experimentalists, including transonic flow, concentrated vortices and dynamic stall. To illustrate the impact of the technological advancements on the way helicopter aerodynamics is studied today, the development of PIV since the early nineties of the last century is reviewed and some rec...
The particle image velocimetry technique (PIV) allows to measure instantaneous flow velocity fields ...
The main interest of today’s research in fl uid mechanics is more and more directed to problems wher...
An experiment was performed on the flap tip vortex shed from a half span Fowler flap. This flap was ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
Particle image velocimetry (PIV) is increasingly used to investigate unsteady velocity fields instan...
Particle Image Velocimetry (PIV) is an important technique to investigate complex flow fields but li...
Detailed studies of the boundary layer profile and the characteristics of the flow velocity distribu...
Particle image velocimetry (PIV) experiments have been performed in order to derive quantitative flo...
The helicopter group at the DLR in Göttingen has been actively involved in the development of measur...
Dynamic stall has proven to be a complex problem in helicopter aerodynamics because it limits the he...
Due to the complexity of the flow field around a helicopter, helicopter aerodynamics deal with quite...
The flow field around a helicopter is characterised by its inherent complexity including effects of...
For the past few years particle image velocimetry (PIV) has been increasingly used for aerodynamic r...
The main interest of todays research in fluid mechanics is more and more directed to problems where ...
For the past few years particle image velocimetry (PIV) has been increasingly used for aerodynamic r...
The particle image velocimetry technique (PIV) allows to measure instantaneous flow velocity fields ...
The main interest of today’s research in fl uid mechanics is more and more directed to problems wher...
An experiment was performed on the flap tip vortex shed from a half span Fowler flap. This flap was ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
Particle image velocimetry (PIV) is increasingly used to investigate unsteady velocity fields instan...
Particle Image Velocimetry (PIV) is an important technique to investigate complex flow fields but li...
Detailed studies of the boundary layer profile and the characteristics of the flow velocity distribu...
Particle image velocimetry (PIV) experiments have been performed in order to derive quantitative flo...
The helicopter group at the DLR in Göttingen has been actively involved in the development of measur...
Dynamic stall has proven to be a complex problem in helicopter aerodynamics because it limits the he...
Due to the complexity of the flow field around a helicopter, helicopter aerodynamics deal with quite...
The flow field around a helicopter is characterised by its inherent complexity including effects of...
For the past few years particle image velocimetry (PIV) has been increasingly used for aerodynamic r...
The main interest of todays research in fluid mechanics is more and more directed to problems where ...
For the past few years particle image velocimetry (PIV) has been increasingly used for aerodynamic r...
The particle image velocimetry technique (PIV) allows to measure instantaneous flow velocity fields ...
The main interest of today’s research in fl uid mechanics is more and more directed to problems wher...
An experiment was performed on the flap tip vortex shed from a half span Fowler flap. This flap was ...