The vortices behind a bluff body equipped with an upswept aft section are studied in a model test. The bluff body operates in close proximity to ground. The principle measurement technique is laser Doppler anemometry (LDA), which is supported by surface flow, pressure and force measurements. The upswept surface has an angle of 17° to horizontal. With the presence of end-plates on the aft section, discontinuities in slope of the force curve exist at several heights in proximity to the ground. The characteristics of these changes are linked with edge vortices. The position and strength of the vortex are identified. Three main types of trailing vortices exist: (a) concentrated, symmetric with a high axial speed core, (b) diffused, symmetric wi...
The near wake of a hitherto untried segmented blunt trailing-edge model has been investigated experi...
This thesis presents an experimental investigation of drag reduction devices on a bluff body in grou...
The influence of the thickness of the boundary layer developing over the surface of an axisymmetric ...
The off-surface aerodynamic characteristics of a wing in ground effect are investigated using a numb...
The off-surface aerodynamic characteristics of a wing in ground effect are investigated using a numb...
The edge vortices generated by a diffuser equipped bluff body in ground effect were experimentally s...
The Ahmed body represents a simplified car of 3D geometry model that can be used to study the flow c...
A study was performed in order to investigate the flowfield characteristics of a wing in ground effe...
The forces and pressures on a generic bluff body in ground effect were investigated. The bluff-body ...
The force and pressure behavior of a generic diffuser in ground effect were investigated. The diffus...
The flow field around simplified bluff bodies constitutes a classic area within vehicle aerodynamics...
The flow field around simplified bluff bodies constitutes a classic area within vehicle aerodynamics...
Introduction The main aerodynamic features which are characteristic for a blunt based bluff body are...
The force and pressure behavior of a generic diffuser in ground effect were investigated. The diffus...
Testing of a 3D bluff body with and without end plate tabs was performed in the California Polytechn...
The near wake of a hitherto untried segmented blunt trailing-edge model has been investigated experi...
This thesis presents an experimental investigation of drag reduction devices on a bluff body in grou...
The influence of the thickness of the boundary layer developing over the surface of an axisymmetric ...
The off-surface aerodynamic characteristics of a wing in ground effect are investigated using a numb...
The off-surface aerodynamic characteristics of a wing in ground effect are investigated using a numb...
The edge vortices generated by a diffuser equipped bluff body in ground effect were experimentally s...
The Ahmed body represents a simplified car of 3D geometry model that can be used to study the flow c...
A study was performed in order to investigate the flowfield characteristics of a wing in ground effe...
The forces and pressures on a generic bluff body in ground effect were investigated. The bluff-body ...
The force and pressure behavior of a generic diffuser in ground effect were investigated. The diffus...
The flow field around simplified bluff bodies constitutes a classic area within vehicle aerodynamics...
The flow field around simplified bluff bodies constitutes a classic area within vehicle aerodynamics...
Introduction The main aerodynamic features which are characteristic for a blunt based bluff body are...
The force and pressure behavior of a generic diffuser in ground effect were investigated. The diffus...
Testing of a 3D bluff body with and without end plate tabs was performed in the California Polytechn...
The near wake of a hitherto untried segmented blunt trailing-edge model has been investigated experi...
This thesis presents an experimental investigation of drag reduction devices on a bluff body in grou...
The influence of the thickness of the boundary layer developing over the surface of an axisymmetric ...