Narayana Rao, CK (1992) Experimental investigation of ejectors as drives for a low speed tunnel. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Experimental studies were carried out with ejectors having 2D and multijet nozzles to determine if they could be adopted to drive a low speed tunnel. A model tunnel was constructed and results obtained from different ejector configurations have been compared. The study suggests that an annular ejector is promising as a candidate configuration for further work leading to an application as a wind tunnel drive.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Ejector;Low speed tunnel |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Experimental Aerodynamics Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 07 Dec 2012 14:14 |
| Last Modified: | 07 Dec 2012 14:14 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11391 |
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