"The purpose of this study will be to conduct a parametric investigation on the performance of elliptic airfoils for Rotor/Wing Unmanned Aerial Vehicles. The objective of this study is to conduct a two-dimensional, aerodynamic analysis on a various elliptic airfoil parameters, compare the reults of the analysis with theoretical predictions and experimental results, and evaluate handling and performance characteristics of Rotor/Wing UAVs during hover, transition, and forward flight"--Abstract, page iii.
Riggins, David W.
Isaac, Kakkattukuzhy M.
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
University of Missouri--Rolla
xii, 105 pages
© 2007 Timothy William Assel, All rights reserved.
Thesis - Open Access
Library of Congress Subject Headings
Aerofoils -- Design
Drone aircraft -- Design and construction
Fluid dynamics -- Data processing
Print OCLC #
Electronic OCLC #
Link to Catalog Recordhttp://laurel.lso.missouri.edu/record=b6430442~S5
Assel, Timothy William, "Computational study of flow over elliptic airfoils for rotor/wing unmanned aerial vehicle applications" (2007). Masters Theses. 4598.