Theoritical evaluation of flow through centrifugal compressor stage

Ramamurthy, S and Rajendran, R and Dilip Kumar, RS (2008) Theoritical evaluation of flow through centrifugal compressor stage. In: International conference for Aerospace Science and Technology , June 2008, Bangalore.

Full text available as:
[img] PDF
Download (1045Kb)

    Abstract

    In this paper a three dimensional viscous flow field in a Centrifugal Impeller with backswept and lean has been numerically analyzed using a commercial code (FLUENT) to understand the physics of complex real flow phenomena. The study was taken to investigate the flow interaction between impeller and vane diffuser for three different setting angles. It was shown at design point the flow at the exit of the impeller is uniform and the classical jet wake pattern is absent. At the intermediate plane between impeller inlet and exit and within vane diffuser channel the flow behaves like a potential flow. The stage analysis carried out using mixing plane formulation for three diffuser settings provided the optimum diffuser setting angle for maximum stage efficiency.

    Item Type: Conference or Workshop Item (Lecture)
    Subjects: AERONAUTICS > Aeronautics (General)
    AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division, Other
    Depositing User: Dr S Ramamurthy
    Date Deposited: 12 Aug 2010 15:12
    Last Modified: 12 Aug 2010 15:12
    URI: http://nal-ir.nal.res.in/id/eprint/8952

    Actions (login required)

    View Item