
Both laminar and turbulent flows are considered. A component analysis is used for the theoretical treatment. The jet flow component is modeled with Schlichting's velocity profile for the laminar case and with Gortler's velocity profile for the turbulence case. The influence of the nozzle exit geometry and the spacing between the radial jet and the flat place is theoretically determined. The equations for the theory are derived, and graphical results are presented
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