Turbulent drag reduction using surface plasma

An experimental investigation has been undertaken in a wind tunnel to study the induced airflow and drag reduction capability of AC glow discharge plasma actuators. Plasma is the fourth state of matter whereby a medium, such as air, is ionized creating a system of electrons, ions and neutral parti...

Full description

Bibliographic Details
Main Author: Jukes, Timothy N.
Format: Thesis (University of Nottingham only)
Language:English
Published: 2007
Subjects:
Online Access:https://eprints.nottingham.ac.uk/12160/
_version_ 1848791446345220096
author Jukes, Timothy N.
author_facet Jukes, Timothy N.
author_sort Jukes, Timothy N.
building Nottingham Research Data Repository
collection Online Access
description An experimental investigation has been undertaken in a wind tunnel to study the induced airflow and drag reduction capability of AC glow discharge plasma actuators. Plasma is the fourth state of matter whereby a medium, such as air, is ionized creating a system of electrons, ions and neutral particles. Surface glow discharge plasma actuators have recently become a topic for flow control due to their ability to exert a body force near the wall of an aerodynamic object which can create or alter a flow. The exact nature of this force is not well understood, although the current state of knowledge is that the phenomenon results from the presence of charged plasma particles in a highly non-uniform electric field. Such actuators are lightweight, fully electronic (needing no moving parts or complicated ducting), have high bandwidth and high energy density. The manufacture of plasma actuators is relatively cheap and they can be easily retrofitted to existing surfaces. The first part of this study aims at characterising the airflow induced by surface plasma actuators in initially static air. Ambient air temperature and velocity profiles are presented around a variety of actuators in order to understand the nature of the induced flow for various parameters such as applied voltage, frequency, actuator geometry and material. It is found that the plasma actuator creates a laminar wall jet along the surface of the material on which it is placed. The second part of the study aims at using plasma actuators to reduce skin-friction drag in a fully developed turbulent boundary layer. Actuators are designed to induce spanwise forcing near the wall, oscillating in time. Thermal anemometry measurements within the boundary layer are presented. These show that the surface plasma can cause a skin-friction drag reduction of up to 45% due to the creation of streamwise vortices which interact with, and disrupt the near-wall turbulence production cycle.
first_indexed 2025-11-14T18:28:38Z
format Thesis (University of Nottingham only)
id nottingham-12160
institution University of Nottingham Malaysia Campus
institution_category Local University
language English
last_indexed 2025-11-14T18:28:38Z
publishDate 2007
recordtype eprints
repository_type Digital Repository
spelling nottingham-121602025-02-28T11:17:53Z https://eprints.nottingham.ac.uk/12160/ Turbulent drag reduction using surface plasma Jukes, Timothy N. An experimental investigation has been undertaken in a wind tunnel to study the induced airflow and drag reduction capability of AC glow discharge plasma actuators. Plasma is the fourth state of matter whereby a medium, such as air, is ionized creating a system of electrons, ions and neutral particles. Surface glow discharge plasma actuators have recently become a topic for flow control due to their ability to exert a body force near the wall of an aerodynamic object which can create or alter a flow. The exact nature of this force is not well understood, although the current state of knowledge is that the phenomenon results from the presence of charged plasma particles in a highly non-uniform electric field. Such actuators are lightweight, fully electronic (needing no moving parts or complicated ducting), have high bandwidth and high energy density. The manufacture of plasma actuators is relatively cheap and they can be easily retrofitted to existing surfaces. The first part of this study aims at characterising the airflow induced by surface plasma actuators in initially static air. Ambient air temperature and velocity profiles are presented around a variety of actuators in order to understand the nature of the induced flow for various parameters such as applied voltage, frequency, actuator geometry and material. It is found that the plasma actuator creates a laminar wall jet along the surface of the material on which it is placed. The second part of the study aims at using plasma actuators to reduce skin-friction drag in a fully developed turbulent boundary layer. Actuators are designed to induce spanwise forcing near the wall, oscillating in time. Thermal anemometry measurements within the boundary layer are presented. These show that the surface plasma can cause a skin-friction drag reduction of up to 45% due to the creation of streamwise vortices which interact with, and disrupt the near-wall turbulence production cycle. 2007-07-13 Thesis (University of Nottingham only) NonPeerReviewed application/pdf en arr https://eprints.nottingham.ac.uk/12160/1/490832.pdf Jukes, Timothy N. (2007) Turbulent drag reduction using surface plasma. PhD thesis, University of Nottingham. Actuators Turbulent boundary layer Skin-friction drag
spellingShingle Actuators
Turbulent boundary layer
Skin-friction drag
Jukes, Timothy N.
Turbulent drag reduction using surface plasma
title Turbulent drag reduction using surface plasma
title_full Turbulent drag reduction using surface plasma
title_fullStr Turbulent drag reduction using surface plasma
title_full_unstemmed Turbulent drag reduction using surface plasma
title_short Turbulent drag reduction using surface plasma
title_sort turbulent drag reduction using surface plasma
topic Actuators
Turbulent boundary layer
Skin-friction drag
url https://eprints.nottingham.ac.uk/12160/