Theses and Dissertations
Issuing Body
Mississippi State University
Advisor
Koenig, Keith
Committee Member
Thompson, David
Committee Member
Hannigan III, Thomas
Date of Degree
8-6-2005
Document Type
Graduate Thesis - Open Access
Major
Aerospace Engineering
Degree Name
Master of Science
College
James Worth Bagley College of Engineering
Department
Department of Aerospace Engineering
Abstract
Design of small uninhabited aerial vehicles is hampered by the relatively sparse database available for aerodynamic properties of basic shapes at low Reynolds number (Re). As a step towards remedying this situation, an experimental investigation of the influence of aspect ratio on the drag of circular cylinders at low Re has been conducted. The experiment itself faced the difficulty of measuring the small forces associated with low Re. A novel solution to this problem has been developed and applied in the Patterson Hall low speed wind tunnel at Mississippi State University. Using this method the drag characteristics of cylinders with aspect ratios varying from 16 down to 1 over a Reynolds number range from 10^5 down to 10^4 have been measured. This presentation will discuss the existing database, the present experimental method and the results that have been obtained.
URI
https://hdl.handle.net/11668/17339
Recommended Citation
Subramanian, Jagdeesh, "Aspect Ratio Effects On Circular Cylinder Drag At Low Reynolds Numbers" (2005). Theses and Dissertations. 734.
https://scholarsjunction.msstate.edu/td/734