Theoretical Evaluation of H.P Turbine Blade profiel sections for GTX-35 VS Engine

Murthy, SJK and Murthy, MVA and Shembharkar, TR (1989) Theoretical Evaluation of H.P Turbine Blade profiel sections for GTX-35 VS Engine. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    High pressure turbine blade profile sections of GTX-35 VS engine were analysed by 2D-Euler code and a boundary layer code employing a (K- E) turbulence model . Computation was carried out to study velocity distribution on the profile surfaces and separation phenomenon for prescribed inlet free stream turbulence . The report presents the results of computation carried out on stator hub, mean and tip sections and rotor, hub and mean sections in detail.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Mach number, Heat transfer coefficient, Turbine cascade, Transonic flow, internal flow, Boundary layer
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division, Propulsion Division
    Depositing User: Ms Indrani V
    Date Deposited: 12 Oct 2012 14:02
    Last Modified: 12 Oct 2012 14:02
    URI: http://nal-ir.nal.res.in/id/eprint/11081

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