Blade-Tip Vortex Noise Mitigation Traded-Off against Aerodynamic Design for Propellers of Future Electric Aircraft

HD Yao, Z Huang, L Davidson, J Niu, ZW Chen - Aerospace, 2022 - mdpi.com
We study noise generation at the blade tips of propellers designed for future electric aircraft
propulsion and, furthermore, analyze the interrelationship between noise mitigation and …

Design and experimental validation of swirl-recovery vanes for propeller propulsion systems

Q Li, K Öztürk, T Sinnige, D Ragni, G Eitelberg… - AIAA Journal, 2018 - arc.aiaa.org
The momentum transferred to the fluid by a running propeller contains not only the desired
axial component but also a rotational component that does not contribute to the propeller …

[HTML][HTML] VR helicity density and its application in turbomachinery tip leakage flows

T Yumeng, LIU Yangwei - Chinese Journal of Aeronautics, 2022 - Elsevier
Helicity is an important quantity that represents the topological interpretation of vortices;
however, helicity is not a Galilean invariant. In this study, VR helicity density (H VR) is …

Aerodynamic and aeroacoustic effects of swirl recovery vanes length

F Avallone, L van den Ende, Q Li, D Ragni… - Journal of Aircraft, 2019 - arc.aiaa.org
A numerical investigation of a propeller with swirl recovery vanes, for which experimental
data exist, is performed. A second swirl recovery vane geometry, with shorter vanes to avoid …

Aerodynamic and aeroacoustic performance of a propeller propulsion system with swirl-recovery vanes

T Sinnige, TCA Stokkermans, D Ragni… - Journal of Propulsion …, 2018 - arc.aiaa.org
Swirl-recovery vanes (SRVs) enhance propulsive efficiency by converting the rotational
kinetic energy in a propeller slipstream into additional thrust. This paper discusses the …

[HTML][HTML] Wing optimization of propeller aircraft based on actuator disc method

Y Zhang, C Haixin, Y Zhang - Chinese Journal of Aeronautics, 2021 - Elsevier
Propeller aircraft are widely used in general aviation. The rotating propeller has a strong
effect on the aerodynamic performance of the wing. This paper uses an actuator disc to …

桨扇恢复旋流叶片优化设计研究

朱磊, 刘汉儒, 陈南树, 王掩刚, 贺象, 赵振国 - 航空动力学报, 2024 - jasp.com.cn
桨扇-恢复旋流叶片(swirl recovery vane, SRV) 结构因其相对对转桨扇结构较为简单的传动机构
, 较弱的叶尖干涉以及能够为推进系统带来推进效率增益而重新受到关注 …

Study on oil-cooler location for a pusher type turbo prop aircraft using numerical simulation

P PS - Aircraft Engineering and Aerospace Technology, 2022 - emerald.com
Purpose Pusher configured turbo-prop aircraft receive inadequate ram air cooling due to the
lack of propeller slipstream, particularly during ground operations. However, flow …

[PDF][PDF] The Contribution of Swirl Recovery to the Induced Drag of Propeller-Wing Systems

R Kooij - 2023 - repository.tudelft.nl
This thesis is written as the final part in the fulfillment of the Master of Science degree in
Aerospace Engineering. After my bachelors, I chose Flight Performance, which fully gratified …

The action mechanism of rotor–stator interaction on the hydraulic and hydroacoustic characteristics of the guide vane in a jet centrifugal pump

R Guo, R Li, R Zhang, W Han - Modern Physics Letters B, 2020 - World Scientific
The aim of this study was to investigate the action mechanism of the rotor–stator interaction
(RSI) in the transient flow field and hydrodynamic noise field of the guide vane in jet …