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Optimisation of Trailing Edge Flaps on the Base Cavity of a Vehicle for Improved Performance at Yaw.

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Bibliographic Details
Title: Optimisation of Trailing Edge Flaps on the Base Cavity of a Vehicle for Improved Performance at Yaw.
Authors: Urquhart, Magnus1 (AUTHOR) magnus.urquhart@volvocars.com, Sebben, Simone1 (AUTHOR)
Source: Flow, Turbulence & Combustion. Aug2022, Vol. 109 Issue 2, p309-326. 18p.
Subjects: Flaps (Airplanes), Greenhouse gas mitigation, Drag (Aerodynamics), Sport utility vehicles, Wind tunnels
Abstract: Regulations to reduce greenhouse gas emissions of passenger vehicles are becoming increasingly stringent. The aerodynamic drag is a major contributor to the vehicle's total energy consumption where a large portion is attributed to the base wake. This paper optimises the angles of small trailing edge flaps on a base cavity of a full-scale sports utility vehicle placed in a wind tunnel. The trailing edge flaps are controlled using servos mounted inside the cavity. The flap angles are optimised using a surrogate model based optimisation algorithm with the objective of reducing the aerodynamic drag at different yaw angles and to create a yaw-insensitive geometry by considering several weighted yaw angles to form the driving cycle averaged drag. Low drag designs are further investigated using base pressures and wake measurements. The results show that the base pressures are symmetrised by reducing the crossflow in the wake. As the model is yawed the wake becomes increasingly downwash dominated by a large rotating windward structure which is reduced by the optimised flaps. The cycle averaged drag optimised design has a smaller increase in drag when yawed compared to a design optimised without considering yaw. [ABSTRACT FROM AUTHOR]
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Database: Engineering Source
Description
Abstract:Regulations to reduce greenhouse gas emissions of passenger vehicles are becoming increasingly stringent. The aerodynamic drag is a major contributor to the vehicle's total energy consumption where a large portion is attributed to the base wake. This paper optimises the angles of small trailing edge flaps on a base cavity of a full-scale sports utility vehicle placed in a wind tunnel. The trailing edge flaps are controlled using servos mounted inside the cavity. The flap angles are optimised using a surrogate model based optimisation algorithm with the objective of reducing the aerodynamic drag at different yaw angles and to create a yaw-insensitive geometry by considering several weighted yaw angles to form the driving cycle averaged drag. Low drag designs are further investigated using base pressures and wake measurements. The results show that the base pressures are symmetrised by reducing the crossflow in the wake. As the model is yawed the wake becomes increasingly downwash dominated by a large rotating windward structure which is reduced by the optimised flaps. The cycle averaged drag optimised design has a smaller increase in drag when yawed compared to a design optimised without considering yaw. [ABSTRACT FROM AUTHOR]
ISSN:13866184
DOI:10.1007/s10494-022-00323-z