CFD investigation of transonic axial compressor rotor blade at various off-design conditions
Flow separation over blade surfaces is an important parameter and its reduction or elimination can improve better aerodynamic performance, efficiency and stall margin. In this work, numerical investigation has been carried out to study the flow separation and performance analysis of a transonic axia...
Main Authors: | Epsipha, Pauline, Zuber, Mohammad, Ahmad, Kamarul Arifin |
---|---|
Format: | Article |
Language: | English |
Published: |
Universiti Putra Malaysia Press
2016
|
Online Access: | http://psasir.upm.edu.my/id/eprint/29375/1/18%20JST%28S%29-0025-2016.pdf |
Similar Items
-
Performance characteristics in transonic axial compressor rotor blade using circular jets
by: Epsipha, Pauline
Published: (2016) -
Wave drag in transonic axial compressors
by: Okurounmu, Olufemi
Published: (2016) -
Computational simulation of unsteady flow in transonic compressor rotor
by: Owen, Philip Ray
Published: (2016) -
Wake behavior downstream of a transonic compressor rotor
by: Stephens, Harry Elias
Published: (2016) -
Exit flow from a transonic compressor rotor
by: Thompkins, William T., et al.
Published: (2016)