Concept of self-excited unsteady flow control on a compressor blade and its preliminary proof by numerical simulation-Reference-Cited by-同舟云学术

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Concept of self-excited unsteady flow control on a compressor blade and its preliminary proof by numerical simulation

Published:2022-04 Issue: Volume:123 Page:107498
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Lu Weiyu^ORCID,Jiao Yanmei,Fu Xin

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. The control of flow separation by periodic excitation;Greenblatt;Prog. Aerosp. Sci.,2000

2. Synthetic jets;Glezer;Annu. Rev. Fluid Mech.,2002

3. Lagrangian analysis on routes to lift enhancement of airfoil by synthetic jet and their relationships with jet parameters;Cao;Aerosp. Sci. Technol.,2020

4. Numerical simulations of high frequency transverse pulsed jet injection into a supersonic crossflow;Williams;Aerosp. Sci. Technol.,2020

5. Flow separation control using unsteady pulsed suction through endwall bleeding holes in a highly loaded compressor cascade;Zhang;Aerosp. Sci. Technol.,2018

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