Aerodynamic drag improvements on a square-back vehicle at yaw using a tapered cavity and asymmetric flaps
Artikel i vetenskaplig tidskrift, 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
Författare
Magnus Urquhart
Chalmers, Mekanik och maritima vetenskaper, Fordonsteknik och autonoma system
Max Varney
Loughborough University
Simone Sebben
Chalmers, Mekanik och maritima vetenskaper, Fordonsteknik och autonoma system
Martin Passmore
Loughborough University
International Journal of Heat and Fluid Flow
0142-727X (ISSN)
Vol. 86 108737 108737Drivkrafter
Hållbar utveckling
Styrkeområden
Transport
Ämneskategorier
Strömningsmekanik och akustik
DOI
10.1016/j.ijheatfluidflow.2020.108737