Flow physics and loss mechanisms of tip leakage flow in variable-blade-pitch-angle ducted fans-Reference-Cited by-同舟云学术

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Flow physics and loss mechanisms of tip leakage flow in variable-blade-pitch-angle ducted fans

Published:2023-11 Issue: Volume:142 Page:108588
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Meijie^ORCID,Cao Yi,Zhou Chao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Review on ducted fans for compound rotorcraft;Zhang;Aeronaut. J.,2020

2. Review of designs and flight control techniques of hybrid and convertible VTOL UAVs;Ducard;Aerosp. Sci. Technol.,2021

3. Variable pitch ducted fans for STOL transport aircraft;Denning,1972

4. Mechanical design of a variable pitch fan for turbofan engines;Violette,2010

5. Design and analysis of passive variable-pitch propeller for VTOL UAVs;Cong;Aerosp. Sci. Technol.,2023

Cited by 2 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. Aerodynamics performance evaluation for new twist angle design axial fan.;Journal of Physics: Conference Series;2024-06-01

2. Numerical and experimental investigations on the aerodynamic and aeroacoustic performance of the blade winglet tip shape of the axial-flow fan;J ACOUST SOC KOREA;2024

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