Modified Lifting Line Method Based on Vortex Rings and Its Application on Lift Fan Design-Reference-Cited by-同舟云学术

Modified Lifting Line Method Based on Vortex Rings and Its Application on Lift Fan Design

Published:2022 Issue:1 Volume:65 Page:23-32
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

WANG Haitong¹,WANG Yangang¹,WANG Siwei¹,ZHOU Fang¹,LIU Hanru¹

Affiliation:

1. School of Power and Energy, Northwestern Polytechnical University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/65/1/65_T-21-10/_pdf

Reference29 articles.

1. 1) Ventura Diaz, P., Caracuel Rubio, R., and Yoon, S.: Simulations of Ducted and Coaxial Rotors for Air Taxi Operations, AIAA Aviation 2019 Forum, Dallas, Texas, 2019-2825, 2019.

2. 2) Platt, R. J.: Static Tests of a Shrouded and an Unshrouded Propeller, NACA RM, No. L7H25, February, 1948.

3. 3) Pereira, J. L. and Chopra, I.: Hover Tests of Micro Aerial Vehicle-scale Shrouded Rotors, Part I: Performance Characteristics, J. Am. Helicopter Soc., 54, 1 (2009), pp. 18–45.

4. 4) Deng, S. and Ren, Z.: Experimental Study of a Ducted Contra-rotating Lift Fan for Vertical/short Takeoff and Landing Unmanned Aerial Vehicle Application, Proceedings of the Institution of Mechanical Engineers, Part G, J. Aerosp. Eng., 232, 16 (2018), 10.

5. 5) Taylor, R. T.: Experimental Investigation of the Effects of Some Shroud Design Variables on the Static Thrust Characteristics of a Small-scale Shrouded Propeller Submerged in a Wing, Technical Report Archive & Image Library, Vol. 8, 1958, pp. 41–50.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aero-propulsion coupling effects and installation characteristics of a distributed propulsion system;Aerospace Science and Technology;2024-10

2. Aero-propulsion analysis of distributed ducted-fan propulsion based on lifting-line driven body-force model;Chinese Journal of Aeronautics;2024-06

3. Aerodynamics Coupling Study on the Tail Cone Electrical Ducted Fan Integrated with Fuselage;2024

4. Aero-Propulsion Analysis of Distributed Ducted-Fan Propulsion Based on Lifting-Line Driven Body-Force Model;2023