Date of Award

Fall 2009

Document Type

Thesis

Degree Name

Master of Science (MS)

Department

Mechanical & Aerospace Engineering

Program/Concentration

Aerospace Engineering

Committee Director

Colin P. Britcher

Committee Member

Thomas Alberts

Committee Member

Drew Landman

Call Number for Print

Special Collections; LD4331.E535 W45 2009

Abstract

This thesis will detail the aerodynamic qualities of a magnetic levitation concept vehicle designed to be installed on Old Dominion University's campus. The vehicle is representative of a class of small, low-speed Maglev systems commonly referred to as Urban Maglev. A 1:12 scale model underwent testing in Old Dominion's low speed wind tunnel. Force and moment coefficients were measured over a wide range of yaw angles. Results give insight into crosswind effects and how these forces affect vehicle dynamics. An analysis of this type is important in understanding the ride quality and safety of the system. Force Coefficients range from 0 - 4 based on vehicle frontal area. Rolling and yawing moment coefficients are significant while the pitching moment is relatively small. The data indicate that at zero degrees (model is facing flow) the axial force is 600 pounds and at 90 degrees yaw (model is perpendicular to flow) the side force can exceed 1300 pounds when both the maximum vehicle and wind speeds are 40 mph. Around 50 degrees unsteadiness develops while the flow structure is changing, and forces at one levitation magnet on the full scale vehicle can reach a peak on the order of 2,400 pounds. The lifting force in a side-wind condition is also relatively large, on the order of 1,500 pounds at an angle between 70 and 90 degrees. These initial results indicate that excessive lift is generated in crosswind conditions. Therefore, simple roof strakes and side skirts were tested, with both modifications successful in reducing the lift force.

Rights

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DOI

10.25777/araz-5681

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