Jayaraman, V (1987) Wind tunnel testing on underwater axisymmetric bodies at angle of attack Part III - Experimental investigation on an axisymmetric Body with Blunt Nose. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
This report, describes the details of the surface pressure measurements made on an axisymmetric body, of finness ratio 15, having blunt nose. The model was tested in the 0.9m dia Low Speed Tunnel at various incidences. The results are presented in this report in the forms of tables and figures.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Wind tunnel testing;Surface pressure measurement;Blunt nose |
| Subjects: | AERONAUTICS > Aerodynamics ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Fluid Mechanics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 25 Jul 2012 11:52 |
| Last Modified: | 25 Jul 2012 11:52 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10649 |
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