Murugesan, K and Sankarnarayana, S and Ramasastry, S (1975) Performance evaluation of a cold-air turning. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Cold Air investigation of a single stage axial turbine13; designed and fabricated at N.A.L., was carried out over a wide range of operating conditions. Using the experimental values obtained, the non dimensional parameters of the turbine were Calculated and the performance graphs were drawn. The estimated values of power and efficiency were compared with the corresponding experimental values at the design conditions. At the design pressure ratio, the13; best operating condition was suggested to get maximum specific power.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Cold air;Axial turbine;Pressure ratio |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Propulsion Division, Propulsion Division, Propulsion Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 10 Nov 2006 |
| Last Modified: | 24 May 2010 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3315 |
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