An experimental investigation was undertaken to measure the effect of various configurations of low-profile vortex generator arrays on the flow in a diffusing S-duct. Three parameters that characterize the vortex generator array were systematically varied to determine their effect: (1) the vortex generator height; (2) the streamwise location of the vortex generator array; and (3) the vortex generator spacing. Detailed measurements of total pressure at the duct exit, surface static pressure, and surface flow visualization were gathered for each vortex generator configuration. These results are reported here along with total pressure recovery and distortion coefficients determined from the experimental data. Each array of vortex generators te...
An experimental study is conducted to determine the dependence of vortex generator geometry and impi...
Performance enhancement of three-dimensional S-duct diffusers by separation control using vortex gen...
Full three-dimensional Navier-Stokes computational results are compared with new experimental measur...
Rectangular S-duct diffusers are widely used in air-intake system of several military aircrafts. A w...
In this paper, results are presented of an experimental investigation into the effectiveness of vort...
Numerical investigations on a diffusing S-duct with/without vortex generators and a straight duct wi...
The development of an effective design strategy for surface-mounted vortex generator arrays in a sub...
The theoretical and experimental work carried out under the NASA/MOD Joint Aeronautical Program has ...
The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is...
An experimental study of the effects of an ingested vortex on the flowfield of a diffusing S-duct is...
The ability of vortex generators (VG) to reduce the unsteady distortion at the exit plane of an S-du...
Performance enhancement of three-dimensional S-duct diffusers by secondary flow and separation contr...
The present study demonstrates that the Reduced Navier-Stokes code RNS3D can be used very effectivel...
Vortex generators within a streamline-traced, external-compression supersonic inlet for Mach 1.66 we...
This paper is a review of significant studies in the complex flow physics in diffusive, s-shaped duc...
An experimental study is conducted to determine the dependence of vortex generator geometry and impi...
Performance enhancement of three-dimensional S-duct diffusers by separation control using vortex gen...
Full three-dimensional Navier-Stokes computational results are compared with new experimental measur...
Rectangular S-duct diffusers are widely used in air-intake system of several military aircrafts. A w...
In this paper, results are presented of an experimental investigation into the effectiveness of vort...
Numerical investigations on a diffusing S-duct with/without vortex generators and a straight duct wi...
The development of an effective design strategy for surface-mounted vortex generator arrays in a sub...
The theoretical and experimental work carried out under the NASA/MOD Joint Aeronautical Program has ...
The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is...
An experimental study of the effects of an ingested vortex on the flowfield of a diffusing S-duct is...
The ability of vortex generators (VG) to reduce the unsteady distortion at the exit plane of an S-du...
Performance enhancement of three-dimensional S-duct diffusers by secondary flow and separation contr...
The present study demonstrates that the Reduced Navier-Stokes code RNS3D can be used very effectivel...
Vortex generators within a streamline-traced, external-compression supersonic inlet for Mach 1.66 we...
This paper is a review of significant studies in the complex flow physics in diffusive, s-shaped duc...
An experimental study is conducted to determine the dependence of vortex generator geometry and impi...
Performance enhancement of three-dimensional S-duct diffusers by separation control using vortex gen...
Full three-dimensional Navier-Stokes computational results are compared with new experimental measur...