Desikan, KS (1972) Slope and deflection of 4-FT.Tunnel model support stings. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
The models for force and pressure measurements in 4-ft. Trisonic Wind Tunnel are generally mounted on stings. For pressure measurements, the model is directly secured on to the sting and for force measurements, the model is supported via a balance mounted on the stings.13;
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Trisonic wind tunnel;Pressure measurements |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 10 Nov 2006 |
| Last Modified: | 24 May 2010 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3345 |
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