The flow field resulting from a single micro-ramp in a Ma=2.0 supersonic boundary layer is investigated using tomographic particle image velocimetry (Tomo-PIV). The measurements were carried out within two volumes behind the micro-ramp. Mean flow characteristics are analyzed, evidence of the streamwise vortex pair is given. In the instantaneous flow, a Kelvin-Helmholtz (K-H) instability developing in the wake of the element is revealed, and the K-H vortices are further identified. A conceptual model is provided to describe the instantaneous flow organization generated by a single micro-ramp
Stereoscopic particle image velocimetry is used to investigate the effects of micro-ramp sub-boundar...
The wake resulting from two micro ramps operating in a supersonic boundary layer at Ma = 2:0 is inve...
Micro-ramps are popular passive flow control devices which can delay flow separation by re-energisin...
The three-dimensional instantaneous flow organization in the near wake of a micro-ramp interacting w...
The micro vortex generator (MVG) is used extensively in low speed aerodynamic problems and is now ex...
The wakes resulting from micro-ramps immersed in a supersonic turbulent boundary layer at Ma = 2.0 a...
Oblique Shock-Wave Reflections or Shock Wave-Boundary Layer interactions (SWBLI) are complex phenome...
The vortical structures in the rear separation and wake region produced by a micro-ramp that immerse...
Micro-ramp vortex generators (or micro-ramps) have gained popularity as promising alternatives to bo...
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propul...
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propul...
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propul...
The flow past a microramp immersed in a supersonic turbulent boundary layer is studied by means of n...
Stereoscopic particle image velocimetry is used to investigate the effects of micro-ramp sub-boundar...
The physical relation between the geometry and the flow topology of the wake of a micro ramp is inve...
Stereoscopic particle image velocimetry is used to investigate the effects of micro-ramp sub-boundar...
The wake resulting from two micro ramps operating in a supersonic boundary layer at Ma = 2:0 is inve...
Micro-ramps are popular passive flow control devices which can delay flow separation by re-energisin...
The three-dimensional instantaneous flow organization in the near wake of a micro-ramp interacting w...
The micro vortex generator (MVG) is used extensively in low speed aerodynamic problems and is now ex...
The wakes resulting from micro-ramps immersed in a supersonic turbulent boundary layer at Ma = 2.0 a...
Oblique Shock-Wave Reflections or Shock Wave-Boundary Layer interactions (SWBLI) are complex phenome...
The vortical structures in the rear separation and wake region produced by a micro-ramp that immerse...
Micro-ramp vortex generators (or micro-ramps) have gained popularity as promising alternatives to bo...
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propul...
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propul...
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propul...
The flow past a microramp immersed in a supersonic turbulent boundary layer is studied by means of n...
Stereoscopic particle image velocimetry is used to investigate the effects of micro-ramp sub-boundar...
The physical relation between the geometry and the flow topology of the wake of a micro ramp is inve...
Stereoscopic particle image velocimetry is used to investigate the effects of micro-ramp sub-boundar...
The wake resulting from two micro ramps operating in a supersonic boundary layer at Ma = 2:0 is inve...
Micro-ramps are popular passive flow control devices which can delay flow separation by re-energisin...