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...

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Bibliographic Details

Published in:	Journal of Applied Fluid Mechanics
Main Authors:	T. Pan, K. Shi, H. Lu, J. Zhang, Q. Li
Format:	Article
Language:	English
Published:	Isfahan University of Technology 2024-10-01
Subjects:	blade sweep transonic compressor rotor aerodynamic loss upstream boundary layer ingestion optimization design
Online Access:	https://www.jafmonline.net/article_2515_827c1ad68241e1f4ce2d33e73c599094.pdf