Aerodynamic drag improvements on a square-back vehicle at yaw using a tapered cavity and asymmetric flaps
Journal article, 2020
The vehicle used is a modified version of the generic Windsor geometry with wheels and a rearward-facing base cavity with nine angled surfaces, or flaps, distributed at the trailing edge of the cavity along the roof and sides. A surrogate model-based optimisation algorithm was used to minimise the drag coefficient by optimising the angle of each flap individually. The experiments were performed in the Loughborough University Large Wind Tunnel. The time-averaged and unsteady results of both the base pressures and tomographic Particle Image Velocimetry indicate that the optimised flap angles improve drag primarily by altering the wake balance. This is achieved by reducing the strength of a large leeward side vortex, reducing the crossflow within the wake.
Drag
Tomographic PIV
Yaw
Aerodynamics
Wake
Optimisation
Crossflow
Author
Magnus Urquhart
Chalmers, Mechanics and Maritime Sciences (M2), Vehicle Engineering and Autonomous Systems
Max Varney
Loughborough University
Simone Sebben
Chalmers, Mechanics and Maritime Sciences (M2), Vehicle Engineering and Autonomous Systems
Martin Passmore
Loughborough University
International Journal of Heat and Fluid Flow
0142-727X (ISSN)
Vol. 86 108737 108737Driving Forces
Sustainable development
Areas of Advance
Transport
Subject Categories
Fluid Mechanics and Acoustics
DOI
10.1016/j.ijheatfluidflow.2020.108737