Sweep Optimization to Reduce Aerodynamic Loss in a Transonic Axial Compressor with Upstream Boundary Layer Ingestion
The aerodynamic performance of axial compressor rotors is negatively affected by the ingestion of boundary layer fluids upstream. As the boundary layer becomes thicker, the blade tip load increases and the local loss is aggravated, especially under off-design operating conditions. The major objectiv...
में बचाया:
| मुख्य लेखकों: | , , , , |
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| स्वरूप: | Artigo |
| भाषा: | Inglês |
| प्रकाशित: |
Isfahan University of Technology
2024-10-01
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| श्रृंखला: | Journal of Applied Fluid Mechanics |
| विषय: | |
| ऑनलाइन पहुंच: | https://www.jafmonline.net/article_2515_827c1ad68241e1f4ce2d33e73c599094.pdf |
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