Simulation Research on a Subsonic Flow around Plane Cascade

Lei Cao; Zheng Heng Zhao; Shu Ying Li

doi:10.4028/www.scientific.net/AMM.419.258

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Simulation Research on a Subsonic Flow around Plane Cascade
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 419Simulation Research on a Subsonic Flow around...

Simulation Research on a Subsonic Flow around Plane Cascade

Abstract:

The paper deals with an analysis of a gas flow through two sets of plane cascade at various angles of attack (0^o, +20^o, -20^o) of different inlet Mach numbers (0.6,0.4, 0.2) by commercial CFD code FLUENT 6.3. Plane cascade aerodynamic research was performed with k-ε model and its flow characteristic was obtained. Its boundary separation and wake were observed. Then their influence factor and development characteristic were studied. Meanwhile, two sets of plane cascade are compared and their aerodynamic characteristics are analyzed.

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Periodical:

Applied Mechanics and Materials (Volume 419)

Pages:

258-263

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.419.258

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Online since:

October 2013

Authors:

Lei Cao, Zheng Heng Zhao, Shu Ying Li

Keywords:

Axial Compressor, Numerical Simulation, Plane Cascade, Subsonic Flow

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