Through flow analysis within axial flow turbomachinery blade rows

Girigoswami, H (1986) Through flow analysis within axial flow turbomachinery blade rows. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    Using Katsani's Through Flow Code, inviscid flow through13; an axial flow compressor rotor blade as well as flow13; through inlet guide vanes are analysed and the computed13; parameters such as meridional velocity distribution, axial velocity distribution along radial lines and velocity distribution over blade surface are presented here.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Through flow
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 24 Jul 2006
    Last Modified: 24 May 2010 09:46
    URI: http://nal-ir.nal.res.in/id/eprint/2180

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