2006
DOI: 10.1007/bf02916279
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Aerodynamic design and analysis of a propeller for a micro air vehicle

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Cited by 4 publications
(3 citation statements)
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“…Early fixed wing MAVs often used commercially available propellers because of their convenience, but peak efficiencies were sometimes as low as 30%. [4][5][6] It was discovered that efficiency could be enhanced by modifying the geometries of these propellers, but these efforts did not lead to significant improvements in the design process. Of the limited studies on MAV propeller design in the literature, most use a vortex theory-based minimum induced loss (MIL) optimization.…”
mentioning
confidence: 99%
“…Early fixed wing MAVs often used commercially available propellers because of their convenience, but peak efficiencies were sometimes as low as 30%. [4][5][6] It was discovered that efficiency could be enhanced by modifying the geometries of these propellers, but these efforts did not lead to significant improvements in the design process. Of the limited studies on MAV propeller design in the literature, most use a vortex theory-based minimum induced loss (MIL) optimization.…”
mentioning
confidence: 99%
“…In Refs. [10,11], practical value ranges for propeller efficiency of the mini and micro aerial aircraft are given. It must be noted that the above equation is written in British units system.…”
Section: Applied Mechanics and Materials Vol 629mentioning
confidence: 99%
“…In the structure design of UAV, the design of propeller is the key to the design of rotor UAV. The aerodynamic performance analysis of the designed propeller is of great significance to the research and improvement of UAV (Lan et al , 2020; Choi, 2012; Cho et al , 2006).…”
Section: Introductionmentioning
confidence: 99%