Investigating the aerodynamic design of a novel tandem fan with a partial-span booster rotor-Reference-Cited by-同舟云学术

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Investigating the aerodynamic design of a novel tandem fan with a partial-span booster rotor

Published:2023-01 Issue: Volume:132 Page:108018
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhou Chuangxin^ORCID,Zhao Shengfeng,Lu Xin'gen

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Influence of circumferential grooves on the aerodynamic and aeroelastic stabilities of a transonic fan;Cong;Aerosp. Sci. Technol.,2021

2. Extending highly loaded axial fan operability range through novel blade design;Lopez;J. Turbomach.,2022

3. Fan stability enhancement with partial casing treatments;Oldfield;J. Turbomach.,2022

4. Performance and flow evolution of windmilling utilizing a combination of semi-empirical speed and CFD models during mode transition of the wide-chord fan;Zhang;Aerosp. Sci. Technol.,2022

5. Numerical investigation of the fan flutter mechanism related to acoustic propagation characteristics;Dong;J. Turbomach.,2022

Cited by 1 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. Investigations on Design Space for Highly Loaded Tandem Bladed Axial Flow Rotor- novel Stator for Low-speed Compressor Research Facility;Journal of Applied Fluid Mechanics;2024-10-01

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