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Boundary layer separation, lift and drag on objects.
Boundary layer separation initiated by the adverse pressure gradient is identified using Large Eddy Simulation.
Results show that both plug-holing and boundary layer separation will influence the natural ventilation performance.
The results reveal that triangular shape vortex generators are best suited to control boundary layer separation.
The boundary layer separation is carefully examined and the vortices shedding mode in each wave period is observed.
This paper presents experimental results of applying surface-suction over the suction-surface of airfoils for controlling boundary layer separation.
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Shear-thickening fluids and body spin accelerate boundary-layer separation.
The developed method allows to calculate flow parameters and energy characteristics of the diffusers and also to estimate the possibility of boundary-layer separation.
The results suggest significant effect of the MSBC and the height on the boundary-layer separation and reattachment, thus affecting the fluid dynamical parameters.
The velocity overshoot in buoyancy aiding flow and flow retardation in opposing flow with early boundary-layer separation are analyzed.
The results suggest that turbulence was generated by flow instabilities and boundary-layer separation, which is analogous to that reported in opposing flow heat transfer studies.
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