Flow control mechanisms of a combined approach using blade slot and vortex generator in compressor cascade

Author:

Hu Jiaguo,Wang Rugen,Huang Danqin

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. Flow control opportunities in gas turbine engines;MacMartin,2000

2. Comparison between synthetic jets and continuous jets for active flow control: application on a NACA 0015 and a compressor stator cascade;De Giorgi;Aerosp. Sci. Technol.,2015

3. Separation control using quasi-radial wall jets;Javadi;Aerosp. Sci. Technol.,2017

4. Flow control using unsteady pulsed holed suction with different excitation models in a highly loaded compressor cascade;Zhang;Proc. Inst. Mech. Eng. A, J. Power Energy,2017

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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