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Wake and surface pressure analysis of vehicles in platoon.

Authors :
Ebrahim, Hesham
Dominy, Robert
Source :
Journal of Wind Engineering & Industrial Aerodynamics. Jun2020, Vol. 201, pN.PAG-N.PAG. 1p.
Publication Year :
2020

Abstract

In this paper, the drag reduction benefits associated with 2 and 3 cars in platoon have been investigated. Following a validation of initial CFD simulations against experimental measurements, predictions of surface pressures and wake structure for alternative platoon configurations have been analysed to determine the changes of flow structure that influence the pressure field and drag force on each vehicle. Contrary to several publications it was found that in a platoon of two vehicles, the drag force of the trailing vehicle exceeded that of an isolated vehicle for close spacings. Analysis of this surprising result revealed that design features introduced to optimise the wake of an isolated vehicle can lead to a drag increase on a following vehicle. For three-vehicle platoons, the flow interaction between the leading and middle vehicles remained largely unchanged but the additional effect of the third vehicle resulted in all three vehicles exhibiting lower drag than that of an isolated vehicle. A clear implication of this work is that results from the analysis of vehicle platoons are likely to be sensitive to the geometry and wake structures of the chosen test vehicle which helps to explain why many previous studies have been seemingly contradictory. Image 1 • Geometrical features optimised for isolated vehicle are detrimental for platoons. • Vertical and lateral stretching of the wake leads to base pressure increase. • The trailing vehicle in a 2-vehicle platoon experiences drag higher than isolation. • All the vehicles in a 3-vehicle platoon show drag reductions. • The leading vehicle in most cases showed the highest drag reduction. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
01676105
Volume :
201
Database :
Academic Search Index
Journal :
Journal of Wind Engineering & Industrial Aerodynamics
Publication Type :
Academic Journal
Accession number :
143119457
Full Text :
https://doi.org/10.1016/j.jweia.2020.104144