Analysis of prancis turbine runner blade channel flow

Murugesan, K (1978) Analysis of prancis turbine runner blade channel flow. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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    Abstract

    An analysis method based on the streamline curvature technique has been discussed for the performance estimation of a pranoic turbine blade channel flow. Some of the numerical problems that could arise in the application of the method are brought forth and modification to the calculating procedure are incorporated so that stable convergences of the solution is obtained. A computer programe based on the method and written for the flow analysis in a general surface of revolution has been used for evaluating a prancis turbine punner blade element.The flow through the blade channel has been anasysed for three different inlet conditions and the performance predicted in the form of outlet velocity trangles and hydroulic efficiency

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Streamline curvature;Turbine blade channel
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 13 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3382

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