Acharya, YVG (1961) Aerodynamic design of a variable mach number supersonic nozzle for the 4'X4' trisonic tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
The methods available for designing supersonic nozzles have been described briefly. The methods, which are considered suitable for designing the variable Mach number nozzle have been discussed in more detail. Examples of the design of the nozzle contour for a particular Mach number by the recommended methods are given.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Supersonic nozzles;Aerodynamic design;Trisonic tunnel |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 19 Jan 2007 |
| Last Modified: | 24 May 2010 09:54 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3774 |
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