Modal analysis of compressor cascades with sweeping jet actuator and pulsed jet for active flow control based on large Eddy simulation
Author:
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference41 articles.
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1. Comparative analysis of corner separation controlled by steady jets and oscillating jets on a compressor cascade;Physics of Fluids;2024-09-01
2. Experimental study on multi-angle pulsed jet actuators for controlling corner separation flow in a compressor cascade;Aerospace Science and Technology;2024-06
3. Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade;Aerospace Science and Technology;2023-11
4. Effects of an unsteady end-wall pulsed jet on a highly loaded compressor cascade at different incidence angles;Physics of Fluids;2023-08-01
5. An unsteady flow control technique based on negative circulation conception and its application to a blade-divergent passage;Frontiers in Energy Research;2023-06-30
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