Masters Theses
Keywords and Phrases
Active flow control
Abstract
"A parametric computational study designed to examine the plausibility of an external body force generated by active means, such as a plasma actuator, as a means of controlling a Laminar Separation Bubble (LSB) over an airfoil at low Reynolds numbers was conducted. Computational Fluid Dynamics (CFD) was employed to characterize the effect that a body force, localized to a small region tangent to the airfoil surface, might have on an LSB. In this study, the effects of altering the strength and location of the "actuator" on the size and location of the LSB and on the aerodynamic performance of the airfoil were observed. In a separate investigation, the effects of operating an actuator in a "burst" mode are investigated, where the effects of pulsing frequency and duty cycle are examined to determine whether further performance enhancements can be achieved via such means. It was found that the body force, when properly located and with sufficient magnitude, could effectively eliminate the LSB. Additionally, it was found that by eliminating the LSB, the aerodynamic efficiency of the airfoil could be improved by as much as 60%. Thus, it was determined that such a system may indeed be an effective measure of reducing or eliminating the negative effects associated with LSBs at low Reynolds numbers. Additionally, pulsed operation of the actuator was found to enhance effectiveness by as much as 20% over a power-equivalent steady actuator. These results indicate that such a control strategy may be an excellent candidate for future experimental research regarding this topic"--Abstract, page iii.
Advisor(s)
Finaish, Fathi
Committee Member(s)
Rovey, Joshua L.
Hosder, Serhat
Department(s)
Mechanical and Aerospace Engineering
Degree Name
M.S. in Aerospace Engineering
Sponsor(s)
Missouri Space Grant Consortium
Publisher
Missouri University of Science and Technology
Publication Date
Summer 2011
Pagination
xv, 97 pages
Note about bibliography
Includes bibliographical references.
Rights
© 2011 Justin Roger Aholt, All rights reserved.
Document Type
Thesis - Open Access
File Type
text
Language
English
Subject Headings
Actuators -- TestingBubblesLaminar flow -- Mathematical modelsPlasma devices -- TestingReynolds number
Thesis Number
T 9799
Print OCLC #
784113545
Electronic OCLC #
745471612
Recommended Citation
Aholt, Justin Roger, "Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles" (2011). Masters Theses. 4977.
https://scholarsmine.mst.edu/masters_theses/4977