High-frequency unsteady flow near the tip in a transonic fan rotor with a small clearance

Author:

Dong XuORCID,Zhang Ziqing,Zhang Yingjie,Zhang Yanfeng,Lu Xingen

Funder

National Science and Technology Major Project

National Natural Science Foundation of China

K. C. Wong Education Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Loss mechanisms in turbomachines;Denton,1993

2. Stall inception and control in a transonic fan, part A: rotating stall inception;Khaleghi;Aerosp. Sci. Technol.,2015

3. The impact of casing groove location on the flow instability in a counter-rotating axial flow compressor;Mao;Aerosp. Sci. Technol.,2018

4. The role of tip leakage flow in spike-type rotating stall inception;Hewkin-Smith;J. Turbomach.,2019

5. Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex;Mailach,2000

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1. Mechanisms of oscillating suction in controlling the tip leakage flow in a high-load compressor cascade;Aerospace Science and Technology;2023-02

2. Uncovering the Root Causes of Stall Flutter in a Wide Chord Fan Blisk;International Journal of Turbomachinery, Propulsion and Power;2022-11-02

3. Combined control of variant clearance and casing aspiration on tip flow field and instability of a transonic compressor;Aerospace Science and Technology;2022-08

4. Attenuation of leakage flow using axially nonuniform tip clearance in high loading transonic compressor rotor;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-05-26

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