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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