Flow structures and aerodynamic behavior of a small-scale joined-wing aerial vehicle under subsonic conditions

Flow behavior and aerodynamic performance of a small-scale joined-wing unmanned aerial vehicle (UAV) was studied experimentally and numerically under various pitch and yaw angle combinations in subsonic flow conditions. Selected numerical results are compared against experimental results obtained us...

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Bibliographic Details
Main Authors: New, Tze How, Teo, Zhen Wei, Li, Shiya, Ong, Z. A., Nagel, Björn
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2023
Subjects:
Online Access:https://hdl.handle.net/10356/171030
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Institution: Nanyang Technological University
Language: English