Velocity distribution over GTX-35-VS HPT stage profiles

Murugesan, K and Ramamurthy, S and Murthy, VVS and Rajendran, R (1990) Velocity distribution over GTX-35-VS HPT stage profiles. Project Report. National Aerospace Laboratories, Bangalore.

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    Surface mach number. Distribution for the hub, mean -and tip profiles of HPT nozzle guide vane(stator), and rotor were theoretically evaluated using compressible flow analysis based on streamline curvature method. The analysis for each profile was carried out for a specified stream tube thickness variation and inlet conditions.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Streamline curvature, compressible flow, surface mach number, velocity distribution
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division, Materials Science Division, Propulsion Division
    Depositing User: Ms Indrani V
    Date Deposited: 06 Dec 2012 09:30
    Last Modified: 19 Aug 2015 10:40

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