Maximum Thickness Location Selection of High Subsonic Axial Compressor Airfoils and Its Effect on Aerodynamic Performance

Maximum Thickness Location Selection of High Subsonic Axial Compressor Airfoils and Its Effect on Aerodynamic Performance

Solidity and camber angle are key parameters with a primary effect on airfoil diffusion. Maximum thickness location has a considerable impact on blade loading distribution. This paper investigates correlations of maximum thickness location, solidity, and camber angle with airfoil performance to choo...

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Bibliographic Details
Main Authors: Chuansijia Tao, Xin Du, Jun Ding, Yizhou Luo, Zhongqi Wang
Format: Article
Language:English
Published: Frontiers Media S.A. 2021-11-01
Series:Frontiers in Energy Research
Subjects:
high subsonic compressor
blade profile
maximum thickness location
solidity
prediction model
database
Online Access:https://www.frontiersin.org/articles/10.3389/fenrg.2021.791542/full

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