Two-Blade UAV Propeller Simulation Case Study
摘要
This study presents the results of tests conducted on a propulsion system, compared with outcomes from computer simulations. The analyzed propeller was scanned using a tomography device, and its geometry was implemented into a simulation program, where the results closely matched the real-world measurements. The conducted case study highlights the significant potential for adapting the propeller to specific applications. The simulation enables low-cost customization of existing solutions to meet the requirements of a given application.