The time mean and turbulence properties of a confined swirling jet using the six orientation, single hot wire technique were obtained. The effect of swirl on a confined, expanding jet is to reduce the size of the corner recirculation zone and generate a central recirculation zone followed by a precessing vortex core. The effect of introducing a contraction nozzle of area ratio four, located two test section diameters downstream of the inlet, is to dramatically reduce the size and shape of the central recirculation zone for the swirling flows considered. The shear stresses are found to increase by an order of magnitude in the region of the contraction nozzle because of large radial gradients of axial velocity. Reduction of the expansion rati...
Convective heat transfer and drying processes are found in industrial applications from gas turbine ...
Convective heat transfer and drying processes are found in industrial applications from gas turbine ...
A computational analysis was performed on the steady, turbulent aerodynamic flowfields associated wi...
The study of circular-to-rectangular transition duct flows with and without inlet swirl is presented...
Experiments were conducted to characterize the time-mean and turbulent flow field of a deflected tur...
Activities undertaken during the entire course of research are summarized. Studies were concerned wi...
The capability and the accuracy of the STARPIC computer code in predicting confined turbulent swirli...
A theoretical and experimental investigation of particle-laden, weakly swirling, turbulent free jets...
Combustor design phenomena; recirculating flows research; single-wire, six-orientation, eddy dissipa...
Fully elliptic forms of the transport equations have been solved numerically for two flow configurat...
A computational method with which to obtain a physical understanding of the turbulent field of two c...
Numerical predictions, flow visualization experiments and time-mean velocity measurements were obtai...
An axisymmetric swirling confined jet flowfield, similar to that encountered in gas turbine combusto...
An engineering prediction method and associated computer code NOZVTX to predict nose vortex shedding...
A recently developed multiple scale turbulence model is used for the numerical prediction of isother...
Convective heat transfer and drying processes are found in industrial applications from gas turbine ...
Convective heat transfer and drying processes are found in industrial applications from gas turbine ...
A computational analysis was performed on the steady, turbulent aerodynamic flowfields associated wi...
The study of circular-to-rectangular transition duct flows with and without inlet swirl is presented...
Experiments were conducted to characterize the time-mean and turbulent flow field of a deflected tur...
Activities undertaken during the entire course of research are summarized. Studies were concerned wi...
The capability and the accuracy of the STARPIC computer code in predicting confined turbulent swirli...
A theoretical and experimental investigation of particle-laden, weakly swirling, turbulent free jets...
Combustor design phenomena; recirculating flows research; single-wire, six-orientation, eddy dissipa...
Fully elliptic forms of the transport equations have been solved numerically for two flow configurat...
A computational method with which to obtain a physical understanding of the turbulent field of two c...
Numerical predictions, flow visualization experiments and time-mean velocity measurements were obtai...
An axisymmetric swirling confined jet flowfield, similar to that encountered in gas turbine combusto...
An engineering prediction method and associated computer code NOZVTX to predict nose vortex shedding...
A recently developed multiple scale turbulence model is used for the numerical prediction of isother...
Convective heat transfer and drying processes are found in industrial applications from gas turbine ...
Convective heat transfer and drying processes are found in industrial applications from gas turbine ...
A computational analysis was performed on the steady, turbulent aerodynamic flowfields associated wi...