The Aerodynamic Effects of the Blade Lean on a High-Aspect-Ratio Transonic Axial Flow Rotor

The Aerodynamic Effects of the Blade Lean on a High-Aspect-Ratio Transonic Axial Flow Rotor

In this study, the effect of tangential blade lean on the aerodynamic characteristics of low-transonic, high-aspect-ratio axial flow compressor rotor has been investigated by using the computational fluid dynamics. The B-Spline curvature with four control points of 25%, 50%, 75% and 100% of span hav...

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Bibliographic Details
Main Authors:	Mansour Asghari, Mohsen Agha Seyed Mirzabozorg, Mahmood Adami
Format:	Article
Language:	English
Published:	Islamic Azad University-Isfahan (Khorasgan) Branch 2018-06-01
Series:	International Journal of Advanced Design and Manufacturing Technology
Subjects:	adiabatic efficiency axial flow compressor cfd high-aspect-ratio low-transonic rotor tangentially leaned
Online Access:	https://admt.isfahan.iau.ir/article_668238_2927ce8152b9f2bc25066f2bd6df2e29.pdf

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