An experimental study of the effects of an ingested vortex on the flowfield of a diffusing S-duct is reported. The vortex is generated through the use of a stationary pinwheel device mounted upstream of the diffusing S-duct. Three test conditions vary the location of the vortex in the duct inlet crossplane. For each condition of ingested vortex, a baseline S-duct and an S-duct with an array of vortex generators is examined. The data taken consist of duct inlet and exit crossplane surveys of velocity and total pressure. Duct surface flow visualization and static pressure are also recorded. The data acquired in these tests are compared to identical S-duct data taken in the absence of the ingested vortex. The ingested vortex is observed to hav...
The use of complex intakes (S-ducts) can enable a closer integration between the airframe and the pr...
A three-dimensional implicit Full Navier-Stokes (FNS) analysis and a 3D Reduced Navier-Stokes (RNS) ...
Complex aero-engine intakes for embedded propulsion systems are expected to play a major role in the...
An experimental investigation was undertaken to measure the effect of various configurations of low-...
Numerical investigations on a diffusing S-duct with/without vortex generators and a straight duct wi...
The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is...
The dynamic flow distortion generated within convoluted aero-engine intakes can affect the performan...
Rectangular S-duct diffusers are widely used in air-intake system of several military aircrafts. A w...
Full three-dimensional Navier-Stokes computational results are compared with new experimental measur...
A Reduced Navier-Stokes (RNS) solution technique was successfully combined with the concept of parti...
The dynamic flow distortion generated within convoluted aeroengine intakes can affect the performanc...
An experimental study of the effect of a vortex ingested into an S-duct diffuser on flow conditions ...
The ability of vortex generators (VG) to reduce the unsteady distortion at the exit plane of an S-du...
Many aircraft employ ducts with centerline curvature or changing cross-sectional shape to join the e...
Convoluted aero-engine intakes are often required to enable closer integration between engine and ai...
The use of complex intakes (S-ducts) can enable a closer integration between the airframe and the pr...
A three-dimensional implicit Full Navier-Stokes (FNS) analysis and a 3D Reduced Navier-Stokes (RNS) ...
Complex aero-engine intakes for embedded propulsion systems are expected to play a major role in the...
An experimental investigation was undertaken to measure the effect of various configurations of low-...
Numerical investigations on a diffusing S-duct with/without vortex generators and a straight duct wi...
The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is...
The dynamic flow distortion generated within convoluted aero-engine intakes can affect the performan...
Rectangular S-duct diffusers are widely used in air-intake system of several military aircrafts. A w...
Full three-dimensional Navier-Stokes computational results are compared with new experimental measur...
A Reduced Navier-Stokes (RNS) solution technique was successfully combined with the concept of parti...
The dynamic flow distortion generated within convoluted aeroengine intakes can affect the performanc...
An experimental study of the effect of a vortex ingested into an S-duct diffuser on flow conditions ...
The ability of vortex generators (VG) to reduce the unsteady distortion at the exit plane of an S-du...
Many aircraft employ ducts with centerline curvature or changing cross-sectional shape to join the e...
Convoluted aero-engine intakes are often required to enable closer integration between engine and ai...
The use of complex intakes (S-ducts) can enable a closer integration between the airframe and the pr...
A three-dimensional implicit Full Navier-Stokes (FNS) analysis and a 3D Reduced Navier-Stokes (RNS) ...
Complex aero-engine intakes for embedded propulsion systems are expected to play a major role in the...