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Numerical Analysis of the Impact of the Interior Nozzle Geometry on Low Mach Number Jet Acoustics
The flow and acoustic fields of subsonic turbulent hot jets exhausting from three divergent nozzles at a Mach number M=0.12 based on the nozzle exit velocity are conducted using a hybrid CFD-CAA method. The flow ...
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Article
Drag Reduction Via Spanwise Transversal Surface Waves at High Reynolds Numbers
The impact of transversal spanwise traveling surface waves on the wall-shear stress distribution of high Reynolds number turbulent boundary layer flows is analyzed using high-resolution large-eddy simulations....