Performance of a Low Speed Axial Compressor Rotor Blade Row under Different Inlet Distortions

Responses of an axial compressor isolated rotor blade row to various inlet distortions have been investigated utilizing computational fluid dynamic technique. Distortions have been imposed by five screens of different geometries, but with the same blockage ratio. These screens were embedded upst...

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Bibliographic Details
Main Authors: R. Taghavi Zenouz, M. Eshaghi Sir, M. H. Ababaf Behbahani
Format: Article
Language:English
Published: Copernicus Publications 2017-05-01
Series:Mechanical Sciences
Online Access:http://www.mech-sci.net/8/127/2017/ms-8-127-2017.pdf