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A Numerical Vortex Approach To Aerodynamic Modeling of SUAV/VTOL Aircraft A Numerical Vortex Approach To Aerodynamic Modeling of SUAV/VTOL Aircraft

by Hunsaker, Douglas F

Abstract (Summary)
A combined wing and propeller model is presented as a low-cost approach to preliminary modeling of slipstream effects on a finite wing. The wing aerodynamic model employs a numerical lifting-line method utilizing the 3D vortex lifting law along with known 2D airfoil data to predict the lift distribution across a wing for a prescribed upstream flowfield. The propeller/slipstream model uses blade element theory combined with momentum conservation equations. This model is expected to be of significant importance in the design of tail-sitter vertical take-off and landing (VTOL) aircraft, where the propeller slipstream is the primary source of air flow past the wings in some flight conditions. The algorithm is presented, and results compared with published experimental data.
Bibliographical Information:

Advisor:

School:Brigham Young University

School Location:USA - Utah

Source Type:Master's Thesis

Keywords:aerodynamic vertical take off and landing vtol suav small aircraft lifting line theory

ISBN:

Date of Publication:12/20/2006

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