Jayaraman, V (1987) Wind Tunnel Testing on Underwater Axisymmetric Bodies at Angle of Attack - Part IV - Surface Pressure Measurements on the Model at Negative Incidences. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
This Project was initiated at the request of NSTL, Vishakapatnam to carryout experimental investigation on an underwater missile configuration having different nose geometry. This paper contains details on the surface pressure measurements carried-out on this model having ogive and blunt noses. 'The model is tested for negative incidences from 0 to 15 deg, at two given wind speeds at 15m and 25m/sec.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Wind tunnel testing;Pressure measurements;Ogive;Blunt noses; Angles of Attack |
| Subjects: | AERONAUTICS > Aerodynamics ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Flight Mechanics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 23 Aug 2012 14:46 |
| Last Modified: | 23 Aug 2012 14:46 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10670 |
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