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: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Turbine cascades, Transonic flow |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Propulsion Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 22 Aug 2012 09:53 |
| Last Modified: | 22 Aug 2012 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10827 |
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