Ramaswamy, MA and Rajendra, G (1978) Experimental investigation of transonic flow past a blunt cone-cylinder. Journal of Spacecraft and Rockets, 15 (2). pp. 120-123. ISSN 0022-4650
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Abstract
The flow past a blunt cone-cylinder at transonic speeds and at moderate angles of incidence has been studied experimentally by recording (1) the longitudinal and circumferential pressure distribution, (2) the surface oil flow patterns using a suspension of titanium dioxide in oleic acid. The results indicate some interesting three-dimensional flow separation phenomenon at transonic speeds.
| Item Type: | Journal Article |
|---|---|
| Additional Information: | Copyright for this article belongs to AIAA |
| Uncontrolled Keywords: | Blunt bodies;Boundary layer separation;Nose cones;Three dimensional cone;Transonic flow;Flow visualization;Pressure distribution;Reynolds number;Shock waves;Titanium oxides; Transonic wind tunnels |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 31 Mar 2010 |
| Last Modified: | 24 May 2010 09:54 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3762 |
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