Development of an experimental setup for propeller performance measurements

With the increasing demand for efficient and adaptable unmanned aerial vehicles (UAVs), optimizing propeller performance has become essential to enhancing energy efficiency and thrust. This study introduces a compact, cost-effective experimental setup designed specifically for testing drone propellers on a small scale, making it accessible for both research and educational applications. The setup integrates off-the-shelf components, including a brushless motor controlled by an electronic speed controller (ESC), a load cell for precise thrust measurement, and a custom-built current sensor for power consumption analysis. The experimental set-up enables real-time data acquisition and evaluation of propeller performance across various operating speeds. By testing two commercial propellers—a two-blade and a three-blade design—the setup demonstrates its ability to analyze thrust and efficiency trends effectively. This innovative framework bridges the gap between theoretical studies and practical UAV applications, providing a versatile and scalable platform for advancing UAV propulsion research.

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Publication Details

Journal
Springer Link (Chiba Institute of Technology)
Published
2025-01-22
DOI
https://doi.org/10.1051/e3sconf/202560802013/pdf
Primary Topic
Advanced Aircraft Design and Technologies
Type
article
Field-Weighted Citation Impact
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article

Development of an experimental setup for propeller performance measurements

Springer Link (Chiba Institute of Technology)
Advanced Aircraft Design and Technologies
article

Development of an experimental setup for propeller performance measurements

article en

Abstract

With the increasing demand for efficient and adaptable unmanned aerial vehicles (UAVs), optimizing propeller performance has become essential to enhancing energy efficiency and thrust. This study introduces a compact, cost-effective experimental setup designed specifically for testing drone propellers on a small scale, making it accessible for both research and educational applications. The setup integrates off-the-shelf components, including a brushless motor controlled by an electronic speed controller (ESC), a load cell for precise thrust measurement, and a custom-built current sensor for power consumption analysis. The experimental set-up enables real-time data acquisition and evaluation of propeller performance across various operating speeds. By testing two commercial propellers—a two-blade and a three-blade design—the setup demonstrates its ability to analyze thrust and efficiency trends effectively. This innovative framework bridges the gap between theoretical studies and practical UAV applications, providing a versatile and scalable platform for advancing UAV propulsion research.

Springer Link (Chiba Institute of Technology)
Technical University of Cluj-Napoca (RO)
Affordable and clean energy
Openalex Percentile: Top 41%
Advanced Aircraft Design and Technologies
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Development of an experimental setup for propeller performance measurements · Springer Link (Chiba Institute of Technology) (2025) | TGRS Research Map | TGRS