Preliminary design and performance analysis of eVTOL propellers using BEMT

Ouedraogo, Boureima and Chen, ZhaoLin and Quino, Cinthia Cielo Gutierrez (2025) Preliminary design and performance analysis of eVTOL propellers using BEMT. International Journal of Science and Research Archive, 15 (2). pp. 345-354. ISSN 2582-8185

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Abstract

Optimizing fixed-pitch propellers for a six-rotor aircraft poses a unique challenge, requiring a balance between high propulsive efficiency during cruise and maximum figure of merit during hover. A low-fidelity Blade Element Momentum Theory (BEMT) model was used to assess the performance of various propeller geometries. Design of Experiments (DOE) with Latin Hypercube Sampling generated 1,000 propeller designs by varying the twist angle while keeping the chord length fixed. The resulting database provides a robust foundation for refining the design through high-fidelity analysis, ensuring optimal performance across multiple flight conditions despite the fixed-pitch constraint.

Item Type: Article
Official URL: https://doi.org/10.30574/ijsra.2025.15.2.1330
Uncontrolled Keywords: eVTOL propeller design; Aerodynamic efficiency; Noise reduction; BEMT; Low-Fidelity Propeller Design
Depositing User: Editor IJSRA
Date Deposited: 22 Jul 2025 23:56
Related URLs:
URI: https://eprint.scholarsrepository.com/id/eprint/1796