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RISComparison of Measured and Computed Flight Performance of a 33-kg Unmanned Aerial Vehicle
Publisher: American Society of Civil Engineers
Abstract: A 32.8-kg unmanned aerial vehicle (UAV) is employed as a case study to assess the accuracy of the empirical techniques used in predicting aerodynamic performance. Despite the prevalent use of empirical methods for the ...
Comparison of Measured and Computed Flight Performance of a 33-kg Unmanned Aerial Vehicle
Publisher: American Society of Civil Engineers
Abstract: A 32.8-kg unmanned aerial vehicle (UAV) is employed as a case study to assess the accuracy of the empirical techniques used in predicting aerodynamic performance. Despite the prevalent use of empirical methods for the ...
Car-Top Test Module as a Low-Cost Alternative to Wind Tunnel Testing of UAV Propulsion Systems
Publisher: American Society of Civil Engineers
Abstract: In an effort to assess motor and propeller performance for small unmanned aerial vehicles (UAVs), a car-top test module has been developed. This device allows for characterization of propeller and motor combinations in ...