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: Monograph (Project Report)
Uncontrolled Keywords: Mach number, Heat transfer coefficient, Turbine cascade, Transonic flow, internal flow, Boundary layer
Subjects: AERONAUTICS > Aircraft Propulsion and Power
Depositing User: Users 10 not found.
Date Deposited: 12 Oct 2012 08:32
Last Modified: 12 Oct 2012 08:32
URI: http://nal-ir.nal.res.in/id/eprint/11081

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