Trailing edge actuation for a bluff body at moderate yaw optimized with a genetic algorithm
Journal article, 2023

This experimental work is conducted to manipulate the wake to reduce aerodynamic drag using the actuations on the trailing edges of a bluff body at a yaw angle of 10°. Two loudspeakers are separately installed into the vertical trailing edges of the vertical base, creating a zero-net mass-flux jet through vertical slots. A maximum drag reduction of 2% and 1.5% is produced by the single actuation on the windward and leeward side, respectively. When the genetic algorithm is introduced to optimize the actuations on both sides, a drag reduction of 7% is obtained. Thus, the energy efficiency of the entire control system is greatly improved by 80% compared to the best single actuation. The underlying flow mechanism behind the effective parameters is proposed according to the analyses of the drag spectra and the hot-wire data measured with and without control. The genetic algorithm provides a promising optimization strategy for the better control performance of trailing edge actuation on a yawed bluff body. Furthermore, this strategy may have the engineering potential to reduce the drag of ground transport vehicles for a large range of operating conditions. Therefore, this research is expected to save energy consumption and improve traveling safety for the aerodynamic control of vehicles.

Author

Zengxi Qiao

Guangzhou Maritime University

Chalmers, Mechanics and Maritime Sciences (M2), Fluid Dynamics

Guglielmo Minelli

Chalmers, Mechanics and Maritime Sciences (M2), Fluid Dynamics

Bernd R. Noack

Harbin Institute of Technology

Technische Universität Berlin

Sinisa Krajnovic

Chalmers, Mechanics and Maritime Sciences (M2)

Valery Chernoray

Chalmers, Mechanics and Maritime Sciences (M2), Fluid Dynamics

Physics of Fluids

10706631 (ISSN) 10897666 (eISSN)

Vol. 35 12 125108

Subject Categories

Aerospace Engineering

Other Engineering and Technologies not elsewhere specified

Vehicle Engineering

Fluid Mechanics and Acoustics

DOI

10.1063/5.0174822

More information

Latest update

3/15/2024