Relative Flow Mach Number Distribution on the Blade PD PR 8606 Profiles of a Turbine Stage

Murthy, MVA and Srinivasa, C (1986) Relative Flow Mach Number Distribution on the Blade PD PR 8606 Profiles of a Turbine Stage. Project Report. National Aerospace Laboratories, Bangalore.

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Abstract

The relative flow Mach number distributions on the surface of stator and rotor blade sections of a turbine stage were determined using the, computer programme COMPBLADE at three radial stations. For the stator blade sections, iso-Mach number contours on the blade to blade surface and the flow Mach number on the blade surface as a function of blade surface length were plotted at the design flow conditions. The rotor profiles were analyzed at the reduced flow Mach numbers, because of, convergence - problem at the design conditions.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Turbine cascades, Transonic flow
Subjects: AERONAUTICS > Aircraft Propulsion and Power
Depositing User: Users 10 not found.
Date Deposited: 22 Aug 2012 04:23
Last Modified: 22 Aug 2012 04:23
URI: http://nal-ir.nal.res.in/id/eprint/10827

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