Int. J. Simul. Multidisci. Des. Optim.
Volume 12, 2021
Simulation and Optimization for Industry 4.0
|Number of page(s)||11|
|Published online||26 August 2021|
Numerical study of new techniques drag reduction: application to aerodynamic devices
Mohammed V University in Rabat, Mohammadia School of Engineering (EMI), Mechanical and Energetic Engineering Research Team: Modelling and Experimentation ERG2 (ME), Avenue Ibn Sina Agdal, Rabat 10090, Morocco
* e-mail: email@example.com
Accepted: 6 August 2021
In the present study, new drag reduction techniques applied to aerodynamic structures have been developed. The test cases have been numerically performed using three simplified models. Simulations have been performed by using the CFD software Ansys fluent. The first case deals with a laminar flow over a flat plate. Drag reduction is obtained by corrugating the shape of the plate. The second case treats a laminar flow over a NACA 0012 airfoil. By the addition of a device fixed on the flow separation point, the drag could be reduced. The last case concerns a turbulent flow over the Ahmed body. Drag reduction is obtained by the perforation of a conduit leading a part of the flow from the front to be injected at the rear of the body.
Key words: Simplified models / drag reduction / flat plate / NACA 0012 / Ahmed body
© A. Agriss et al., published by EDP Sciences, 2021
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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