The aerodynamic behavioral study of tandem fan wing configuration

D Siliang, T Zhengfei - International Journal of Aerospace …, 2018 - Wiley Online Library
The fan wing aircraft is a new concept based on a new principle, especially its wing which is
based on a unique aerodynamic principle. A fan wing can simultaneously generate lift and …

Experimental and numerical study of an airfoil in combination with a cross flow fan

S Askari, MH Shojaeefard - Proceedings of the Institution of …, 2013 - journals.sagepub.com
In this article, the airfoil comprising a cross flow fan has been studied at various boundary
conditions by experiment and numerical solution. The airfoil generates high lift at low …

Research on Aerodynamic Test Validation and the Vector Force Control Method for an E-STOL Fan Wing Unmanned Aerial Vehicle

S Du, Y Zha, Q Zhao - Aerospace, 2024 - mdpi.com
The concept of the Fan Wing, a novel aircraft vector-force-integrated device that combines a
power unit with a fixed wing to generate distributed lift and thrust by creating a low-pressure …

Study on Helicopter Antitorque Device Based on Cross‐Flow Fan Technology

D Siliang, T Zhengfei, X Pei… - International Journal of …, 2016 - Wiley Online Library
In order to improve low‐altitude flight security of single‐rotor helicopter, an experimental
model of a helicopter antitorque device is developed for wind tunnel test. The model is …

Numerical Simulation of the Effect of Different Number Leading Edge Winglets on the Fan‐Wing Aerodynamic Characteristics

D Siliang, Z Qijun, T Zhengfei - International Journal of …, 2020 - Wiley Online Library
The generation of lift and thrust mainly depends on the formation of low‐pressure vortices
above the arc groove on the leading edge of the Fan‐wing, which makes the lift and thrust …

Effect of blade parameters on lift performance of drum-type vertical cross-flow fan

S Wang, X Wang, H Chen, Z Qiu - Journal of Physics: Conference …, 2024 - iopscience.iop.org
The drum-type vertical cross-flow fan represents a novel approach to fan-wing technology.
By re-configuring the traditional cross-flow fan in a vertical orientation, the symmetrical end …

[引用][C] 扇翼飞行器的研究进展与应用前景

孟琳, 叶永强, 李楠 - 航空学报, 2015

[PDF][PDF] Experimental and numerical study of the aerodynamics of a cross flow fan embedded wing configuration

C Coskunses, O Tuncer - Journal of the Faculty of Engineering …, 2022 - scholar.archive.org
Experimental and numerical study of the aerodynamics of a cross flow fan embedded wing
configuration Page 1 Journal of the Faculty of Engineering and Architecture of Gazi University …

Performance optimization of a novel wing integrated distributed propulsion systems

S Durmaz, O Alahmad, BH Saracoglu - 2018 AIAA Aerospace Sciences …, 2018 - arc.aiaa.org
I. Introduction nlike conventional and contemporary propulsion systems where thrust
generation is localized within a close proximity to the engines, distributed propulsion offers a …

基于扇翼机翼升推力机理的吹气机翼研究

杜思亮, 唐正飞 - 航空动力学报, 2017 - jasp.com.cn
基于对扇翼飞行器升推力产生机理的数值计算与分析, 提出了一种扇翼飞行器机翼的替代方案——
吹气机翼. 分析了扇翼机翼升推力的产生机理并在扇翼机翼翼型的基础上构建了吹气机翼翼型 …