Comparison of Computational Approaches for Rapid Aerodynamic Assessment of Small UAVs

Author:

Shafer Theresa1,Viken Sally2,Favaregh Noah M.2,Zeune Cale H.3,Williams Nathan4,Dansie Jonathan5

Affiliation:

1. Naval Air Systems Command

2. NASA Langley Research Center

3. Air Force Research Laboratory

4. Defence Technology Agency

5. Australian National University

Publisher

American Institute of Aeronautics and Astronautics

Reference18 articles.

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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2. Low-Fidelity Aerodynamic Computational Simulation on a Fixed Wing-Multirotor Hybrid Unmanned Aerial Vehicle;J AERONAUT ASTRONAUT;2023

3. Flight controller design and Geometric Parameter Optimization for a Tandem Wing UAV;2023 3rd International conference on Artificial Intelligence and Signal Processing (AISP);2023-03-18

4. Unsteady Aerodynamic Response of the Kahu UAV Wing under Turbulent Conditions;AIAA AVIATION 2021 FORUM;2021-07-28

5. Aerodynamic Investigations of UAV Sensor Turrets - A Combined Wind-tunnel and CFD Approach;AIAA Scitech 2021 Forum;2021-01-04

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