Study of quadcopter propellers at low Reynolds number

Study of quadcopter propellers at low Reynolds number

During horizontal flight the propellers of quadcopter is working in oblique flow conditions. This case not studied enough for fixed pitch propellers especially at low Reynolds numbers, which are implemented on propellers of small quadcopters. The experimental investigation of characteristics of thre...

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Hauptverfasser: Markin, V. V., Polivanov, P. A.
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Sprache:eng
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Computational fluid dynamics
Fluid flow
Helicopters
Horizontal flight
Propellers
Reynolds number
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Polivanov, P. A.
description During horizontal flight the propellers of quadcopter is working in oblique flow conditions. This case not studied enough for fixed pitch propellers especially at low Reynolds numbers, which are implemented on propellers of small quadcopters. The experimental investigation of characteristics of three-blade propeller for quadcopter in different conditions (including oblique blowing) was carried out. The effect of oblique flow mode on the dimensionless characteristics of the propeller was investigated. The unsteady component of the force generated by the propeller was estimated on the basis of numerical simulation.
doi_str_mv 10.1063/5.0052228
format Conference Proceeding
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identifier ISSN: 0094-243X
ispartof AIP conference proceedings, 2021, Vol.2351 (1)
issn 0094-243X
1551-7616
language eng
recordid cdi_scitation_primary_10_1063_5_0052228
source AIP Journals Complete
subjects Computational fluid dynamics
Fluid flow
Helicopters
Horizontal flight
Propellers
Reynolds number
title Study of quadcopter propellers at low Reynolds number
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