Jul 2026· Theoretical and Natural Science· Vol 180, pp. 204-213· 0 citations
Abstract
Low pressure wake behind the body of a vehicle is the most important component of its aerodynamic drag at highway speeds, not the viscous friction along the body. In typical scales for vehicles, the Reynolds number is O ( 1 0 6 ) , which means that the boundary layer is turbulent and stays attached for the major part of the front and roof of the vehicle. The major problem is at the back where there is an adverse pressure gradient and the flow has a tendency to separate. So automotive drag is a more complex subject that is more related to a mechanism chain and not necessarily to speed. After separation a detached shear layer rolls up into coherent structures and a recirculating wake is formed. This wake size and structure will influence the mean base pressure and thus the drag. Based on the canonical Ahmed model, boundary-layer theory, separation criteria and wake scaling are used to demonstrate the order of variation in drag relative to relatively small changes in the rear geometry. From this point of view, the effective way of drag reduction is not to avoid separation, but to control the development of the separated wake and to enhance the pressure recovery.
Motivated by the substantial contribution of the wheel region to ground-vehicle aerodynamic drag, the present study examines flow around a circular cylinder inside a straight-curved hybrid channel as a reduced-order representation of the coupled wheel-ground-housing system. Large-eddy simulations are employed to quanti...
Qian-Wen Zhang, Tao Huang, Qing-Yang Wang et al.· The Physics of Fluids· 0 citations
The dynamics and transitions of the flow past a square cylinder sliding along a wall are investigated numerically for Reynolds numbers (Re) between 20 and 300, and gap distances (G) between 0.05 and 1.0 side length of the square (D). The presence of the wall is found to fundamentally alter the wake dynamics and three-d...
Zhi-Jiang Yuan, Xiao Jiang, Ming-Dong Lv et al.· The Physics of Fluids· 0 citations
The aerodynamic performance of conventional (rounded leading-edge) and reversed (sharp leading-edge) airfoils is investigated in the low Reynolds number regime. Computations are performed in the range Re ∈ [1x108, 8x104]. The results show significant differences in the flow structures and the aerodynamic characteristic...
T. Grishma, Kavya Nagaraj, M. Sivapragasam· Journal of aerospace science...· 0 citations
Abstract Content of image described in text. Pipe flow controlled by streamwise-travelling waves of azimuthal wall velocity is studied using direct numerical simulations at a bulk Reynolds number italic Re Subscript b Baseline equals 4900 Reb=4900
$\textit{Re}_b=4900$
. A comprehensive analysis of drag reduction shows...
E. Gallorini, D. Massaro, Philipp Schlatter et al.· Journal of Fluid Mechanics· 0 citations
Depending on the counter-flow jet (CFJ) injection characteristics, the flow field can be classified into the short penetration mode (SPM) and the long penetration mode. Although SPM is generally considered stable, the pressure drag coefficient exhibits significant fluctuations exceeding 10%, which cannot be explained b...
H. Yoon, In-Seuck Jeung· The Physics of Fluids· 0 citations
Trailing-edge (TE) serrations serve as an effective flow control strategy with the superior wake-flow adaptability. While existing studies are mainly focused on overall aerodynamic benefits of blade cascade, the underlying wake/vortex control mechanisms, particularly the effects of serration spanwise positions, remain...
Wen-Jun Yang, Ying Zhan, Yin-Hao Wang et al.· The Physics of Fluids· 0 citations
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