Sridhara, K and Thunga, KS (1974) Design and development of a cold air turbine. Technical Report. National Aerospace Laboratories, Bangalore,India.
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Abstract
A high speed drive unit with a continuosly variable speed power characteristics is a necessary tool for testing protype compressors and fans and high speed bearings.Such a drive unit is a special purpose machine and is generally not available in the normal range of compressed air is already available at National Aeronautical Laboratory,it was decided to develop a compact cold gas turbine of jet engines was available from the Airforce disposal stock which formed the basis for the design of the turbine
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | High speed drive;Protype compressors;Industrial electric machine |
| Subjects: | ENGINEERING > Engineering (General) |
| Division/Department: | Propulsion Division, Propulsion Division |
| Depositing User: | shankar sk nadoor |
| Date Deposited: | 14 Nov 2006 |
| Last Modified: | 24 May 2010 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3399 |
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