Abstract
The effect of boundary layer oscillating suction (BLOS) on the vortex structure of high-load linear compressor cascades is studied by a high-fidelity numerical calculation. The oscillation parameters (amplitude and frequency) and suction control parameters (suction position and mass flow) are continuously adjusted. It was found that higher aerodynamic efficiency could be obtained with suitable oscillation parameters and suction control parameters. This is achieved because BLOS not only absorbs the low-energy fluid in the boundary layer but also optimizes the vortex structure in the compressor passage.
| Original language | English |
|---|---|
| Article number | 989883 |
| Journal | Frontiers in Energy Research |
| Volume | 10 |
| DOIs | |
| State | Published - 21 Sep 2022 |
| Externally published | Yes |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- boundary layer
- compressor cascade
- oscillating suction
- separated flow control
- vortex structure
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