Influence of yaw on propeller aerodynamic characteristics
University of Defence, Kounicova 65, 66210, Brno, Czech Republic
2 Military Technical Academy, Hoang Quoc Viet 236, Hanoi, Vietnam
* Corresponding author: firstname.lastname@example.org
Published online: 4 June 2018
Between the propeller axis and free stream direction, it can still be a non-zero yaw angle. This paper introduces some propeller experiments, in which the propeller aerodynamic characteristics have been determined in various yaw angle and different rotational speeds. The experimental aerodynamic characteristics are acquired dynamic values, from which the influence of yaw conditions on the frequency and the amplitude of propeller thrust and torque can be obtained.
© The Authors, published by EDP Sciences, 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. (http://creativecommons.org/licenses/by/4.0/).