Chidananda, MS and Jaganatha Rao, B and Venkatesh, S and Krishna Kumar, VS and Davis, A (1995) Performance of GTX- 35 VS Engine Scaled Nozzles. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Scaled models of the GTX-35 VS engine convergent nozzles were tested under simulated . conditions with particular reference to nozzle discharge and thrust coefficients . Nozzles having half angles of 7 ° , 12 ° , 22°, 30° and 35 ° were tested at pressure ratios varying upto 10 . Reynolds numbers at inlet to the test nozzles were of same order as those found in the engine . The results obtained were in broad agreement with the data available in literature and were found to be satisfactory.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Propulsive nozzle; Nozzle thrust, discharge coefficient, thrust coefficient |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division, Other |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 15 Nov 2012 11:13 |
| Last Modified: | 15 Nov 2012 11:13 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11357 |
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