TY  - JOUR
AU  - Svorcan, Jelena
AU  - Wang, Jonathan M.
AU  - Griffin, Kevin Patrick
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3724
AB  - Successful flow control may bring numerous benefits, such as flow stabilization, flow reattachment, separation delay, drag reduction, lift increase, aerodynamic performance improvement, energy efficiency increase, shock delay or weakening, noise reduction, etc. For these purposes, many different flow control devices, which can be classified as passive, semi-active and active, have been designed and tested. This review paper aims to highlight the most promising and commonly employed boundary layer control methods as well as outline their potential in specific applications in aerospace and energy engineering. Referenced studies, performed on various geometries (flat plates, channels, airfoils, wings, blades, cylinders), are primarily numerical or experimental. Although enhanced aerodynamic performance is achieved in many cases, further research is required to draw general conclusions. This paper aims to demonstrate that, in the future, we may expect further developments of flow control actuators, as well as their increased application.
PB  - Sage Publications Ltd, London
T2  - Advances in Mechanical Engineering
T1  - Current state and future trends in boundary layer control on lifting surfaces
IS  - 7
VL  - 14
DO  - 10.1177/16878132221112161
ER  - 

@article{
author = "Svorcan, Jelena and Wang, Jonathan M. and Griffin, Kevin Patrick",
year = "2022",
abstract = "Successful flow control may bring numerous benefits, such as flow stabilization, flow reattachment, separation delay, drag reduction, lift increase, aerodynamic performance improvement, energy efficiency increase, shock delay or weakening, noise reduction, etc. For these purposes, many different flow control devices, which can be classified as passive, semi-active and active, have been designed and tested. This review paper aims to highlight the most promising and commonly employed boundary layer control methods as well as outline their potential in specific applications in aerospace and energy engineering. Referenced studies, performed on various geometries (flat plates, channels, airfoils, wings, blades, cylinders), are primarily numerical or experimental. Although enhanced aerodynamic performance is achieved in many cases, further research is required to draw general conclusions. This paper aims to demonstrate that, in the future, we may expect further developments of flow control actuators, as well as their increased application.",
publisher = "Sage Publications Ltd, London",
journal = "Advances in Mechanical Engineering",
title = "Current state and future trends in boundary layer control on lifting surfaces",
number = "7",
volume = "14",
doi = "10.1177/16878132221112161"
}

Svorcan, J., Wang, J. M.,& Griffin, K. P.. (2022). Current state and future trends in boundary layer control on lifting surfaces. in Advances in Mechanical Engineering
Sage Publications Ltd, London., 14(7).
https://doi.org/10.1177/16878132221112161

Svorcan J, Wang JM, Griffin KP. Current state and future trends in boundary layer control on lifting surfaces. in Advances in Mechanical Engineering. 2022;14(7).
doi:10.1177/16878132221112161 .

Svorcan, Jelena, Wang, Jonathan M., Griffin, Kevin Patrick, "Current state and future trends in boundary layer control on lifting surfaces" in Advances in Mechanical Engineering, 14, no. 7 (2022),
https://doi.org/10.1177/16878132221112161 . .