Narayanamurthy, RS (1973) Determination of aerodynamic nozzle contours for transonic cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
In this report a procedure suitable for obtaining the potential aerodynamio contours of a nozzle and the necessary boundary layer corrections is described. After a description of the method, the procedure for computerising the above calculations by the said method is presented.13; The method is then used to obtain the potential flow contours of the nozzle with necessary boundary layer corrections.These are contours are proposed to be used in the transonic cascade wind Tunnel.These coi1tours13; The results obtained for various test section heights and flow Mach numbers are presented.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aerodynamic nozzle;Transonic cascade tunnel |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 07 Nov 2006 |
| Last Modified: | 24 May 2010 04:23 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3312 |
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