The Design of a Wind Tunnel Testing System for Model Airborne Wind Energy Systems

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2020
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Swarthmore College. Dept. of Engineering
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en
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Full copyright to this work is retained by the student author. It may only be used for non-commercial, research, and educational purposes. All other uses are restricted.
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In the last decades there has been rapid growth of renewable energy technologies in lout of societies increased energy demand. Among these technologies, wind generators are among the most widely used type of energy harvester, in particular large wind turbines. However, wind turbines require large areas of land and extensive support structures. For this reason, there has been substantial focus on the development of Airborne Wind Energy Systems (AWES) due to their high potential of power capacity per unit of land area. My E90 project focuses on a particular subset of AWES that utilizes kites to drive a generator on the ground. The goal of this project is to design a testing system in the Singer wind tunnel to measure the force, potential energy generated, and flight dynamics of various kite designs. In addition to the system design, characterization of the flow velocity and uniformity of the Singer wind tunnel is included in this report. In this work, I provide an overview of the system design and its sub-components and lay out a framework for fabrication and implementation.
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