The interaction of a turbulent boundary layer on a flat plate with a strong artificially generated longitudinal vortex which may or may not actually enter the boundary layer is studied. The vortices are generated by a delta wing suspended ahead of the test plate, so that the configuration is approximately that of a close coupled carnard with zero main-wing sweep and an invisible body. All necessary configuration and parametric checks are completed, and data acquisition and analysis on the first configuration chosen for detailed study, in which the vortex starts to merge with the boundary layer a short distance downstream of the leading edge of the test plate, are nearly complete
PIV experiments were conducted in the wake of an aspect ratio 4 flat plate at the University of Dayt...
The effects of leading edge flaps on the aerodynamic characteristics of a low aspect-ratio delta win...
Streamwise vortices can be observed to interact in a number of real world scenarios. Vortex generato...
The interaction of a turbulent boundary layer (on a flat plate) with a strong artificially-generated...
The second test case (longitudinal vortex above, but not merging with, a turbulent boundary layer) w...
This report summarizes the work done under NASA Grant NAGw-581, Vortex/Boundary Layer Interactions. ...
An experimental study was conducted to examine the interaction between a single weak streamwise vort...
An experimental investigation has been carried out to study and understand the influence of an end p...
Direct drag measurements were obtained on a flat plate with a spanwise row of vortex generators near...
The main objective of the present study is to experimentally investigate interactions between a long...
Helium bubble flow visualizations have been performed to study perpendicular interaction of a turbul...
Unsteady aerodynamics of nonslender delta wings, covering topics of shear layer instabilities, struc...
Work is devoted to study of free-stream vorticity normal to leading edge interaction with boundary l...
The interaction of a spanwise vortex with a flat plate was investigated experimentally in a wind tun...
Vortex interaction with a thick elliptical leading-edge at zero relative offset produces a pronounce...
PIV experiments were conducted in the wake of an aspect ratio 4 flat plate at the University of Dayt...
The effects of leading edge flaps on the aerodynamic characteristics of a low aspect-ratio delta win...
Streamwise vortices can be observed to interact in a number of real world scenarios. Vortex generato...
The interaction of a turbulent boundary layer (on a flat plate) with a strong artificially-generated...
The second test case (longitudinal vortex above, but not merging with, a turbulent boundary layer) w...
This report summarizes the work done under NASA Grant NAGw-581, Vortex/Boundary Layer Interactions. ...
An experimental study was conducted to examine the interaction between a single weak streamwise vort...
An experimental investigation has been carried out to study and understand the influence of an end p...
Direct drag measurements were obtained on a flat plate with a spanwise row of vortex generators near...
The main objective of the present study is to experimentally investigate interactions between a long...
Helium bubble flow visualizations have been performed to study perpendicular interaction of a turbul...
Unsteady aerodynamics of nonslender delta wings, covering topics of shear layer instabilities, struc...
Work is devoted to study of free-stream vorticity normal to leading edge interaction with boundary l...
The interaction of a spanwise vortex with a flat plate was investigated experimentally in a wind tun...
Vortex interaction with a thick elliptical leading-edge at zero relative offset produces a pronounce...
PIV experiments were conducted in the wake of an aspect ratio 4 flat plate at the University of Dayt...
The effects of leading edge flaps on the aerodynamic characteristics of a low aspect-ratio delta win...
Streamwise vortices can be observed to interact in a number of real world scenarios. Vortex generato...