Abstract
Rotor-powered drones continue to grow in popularity in private and government sectors. The use of these drones in challenging environments and in high stakes applications calls for a certain level of robustness and redundancy. Often, these drones are equipped with sets of paired coaxial rotors, which not only improve the performance of the vehicle, but also ensure that a failure of one motor does not constitute the failure of the whole vehicle. Some applications such as extraterrestrial exploration, which use these coaxial rotors, can benefit from a wing shaped rotor arm to reduce drag and increase lift, extending mission lifetime. This work explores the design of one such coaxial rotor-wing system, using computational fluid dynamics to assess the system performance in a pair of flight conditions. Various parameters of the wing design are adjusted to ascertain the optimal configuration to satisfy various performance criteria.
Notes
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Graduation Date
2021
Semester
Summer
Advisor
Kinzel, Michael
Degree
Master of Science in Aerospace Engineering (M.S.A.E.)
College
College of Engineering and Computer Science
Department
Mechanical and Aerospace Engineering
Degree Program
Aerospace Engineering; Thermofluid Aerodynamic Systems
Format
application/pdf
Identifier
CFE0008759; DP0025490
URL
https://purls.library.ucf.edu/go/DP0025490
Language
English
Release Date
8-15-2021
Length of Campus-only Access
None
Access Status
Masters Thesis (Open Access)
STARS Citation
Yeager, Tadd, "Optimization of a Wing Supporting a Coaxial Rotor for Multiple Flight Conditions" (2021). Electronic Theses and Dissertations, 2020-2023. 788.
https://stars.library.ucf.edu/etd2020/788