Turbine test facility of Propulsion Division

Murthy, MVA and Paranjpe, PA (1977) Turbine test facility of Propulsion Division. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Development of turbine test facility in the propulsion division of NAL Bangalore was initiated in 1970.This facility is intended to carry out performance evaluation of model turbine stages and to generate stage design data which would be useful in the development of full-scale turbines.In edition,the rotating stage data would provide a measure of correlation with cascade.this report deals with the detailed description of the test facility and its capabilities.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Turbine test;Rotating stage
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Propulsion Division, Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 09 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3310

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