[HTML][HTML] An investigation of tip vortices unsteady interaction for Fokker 29 propeller with swirl recovery vane

Q Li, Y Wang, G Eitelberg - Chinese Journal of Aeronautics, 2016 - Elsevier
A numerical study was performed to explore the unsteady interaction between the upstream
propeller and the downstream swirl recovery vane (SRV) by transient simulations. Much …

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 …

Pressure field measurements on large-scale propeller blades using pressure-sensitive paint

C Wei, L Jiao, F Tong, Z Chen, Y Liu, D Peng - Acta Mechanica Sinica, 2022 - Springer
Pressure-sensitive paint (PSP) is a global pressure measurement technique. Compared with
pressure transducers, PSP has significant advantages such as high spatial resolution and a …

A CFD mesh independent solution technique for low Reynolds number propeller

A Seeni, P Rajendran, H Mamat - 2021 - akademiabaru.com
There are several techniques available for finding mesh independent solutions in
Computational Fluid Dynamics (CFD) problems. The most commonly known methods are …

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 …

[PDF][PDF] Mitigation of propeller kinetic energy losses with boundary layer ingestion and swirl recovery vanes

TCA Stokkermans, N Van Arnhem… - Proceedings of the …, 2016 - researchgate.net
In order to improve the efficiency of propeller propulsion systems, two existing ideas for
mitigation of the kinetic energy losses and the resulting aerodynamic interactions are …

涵道桨定子气动增效和消旋效应的分析与验证

李卓远, 杨旭东, 屈丽娟, 孙恺 - 航空动力学报, 2025 - jasp.com.cn
桨后定子是影响涵道螺旋桨推进效率, 转矩抵消和桨后滑流整流效应的重要部件之一,
为研究桨后定子对气动推进增效, 消旋及桨后滑流整流效应的桨后定子构型气动综合设计和参数 …