“…Many theoretical, experimental, and numerical studies are performed in these aspects to analyze wake structure under the effects of different parameters. Researchers (Gad-el-Hak, 2000;Salmasi et al, 2013;Mohammadi and Taleghani, 2014;Abdolahipour et al, 2022a;Rahni et al, 2022;Shams Taleghani and Sheikholeslam Noori, 2022) investigated flow control basics and strategies to achieve transition delay, detachment prevention, lift augmentation, drag reduction, vortex suppression, noise reduction, and heat and mass transfer enhancements. Taleghani, A. S., et al (Bajalan et al, 2011;Mirzaei et al, 2012;Taleghani et al, 2018;Noori et al, 2020;Abdolahipour et al, 2021;Noori et al, 2021;Abdolahipour et al, 2022a;Abdolahipour et al, 2022b) investigated different phenomena like ionic wind velocity in quiescent air at atmospheric pressure caused by a dielectric barrier discharge plasma actuator, effect of modulated pulse jet vortex generator, Enhancing pressure on a supercritical high-lift wing by applying a Modular and Simple Pulse Jet Vortex Generator, flow field properties of a baseline single pulsed jet actuator, airfoil's active flow control using a plasma actuator, acoustic streaming in a drop created by surface acoustic waves, a sessile drop's dynamic behavior, and behavior of a circular cylinder with an airfoil through experimental methods.…”