Desai, SS and Sharma, Ramachandra and Venkateshwarlu, K and Krishnamurthy, K (1982) Wall interference studies on NACA 0012 Aerofoil in the NAL 0.3m wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Experimental investigations were carried out on a 150mm chord NACA 0012 aerofoil in the NALls O.3m Trisonic Wind Tunnel with its transonic liners set at a open-area-ratio (OAR) around 2%. These tests confirm the earlier conclusion, derived from tests on a BGK (supercritical) aerofoil, that a 2% OAR for this tunnel produces distribution free, correctable results in the transonic regime, upto Mach number of about 0.8. As a support to the conclusion comparisons are also presented with the results of NPL (England).
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Number comparison;OAR;Trisonic wind tunnel |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics, Aerodynamics, Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 30 Aug 2006 |
| Last Modified: | 24 May 2010 09:49 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2575 |
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