Experimental investigation of transonic flow past a blunt cone-cylinder

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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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: 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
Depositing User: Users 90 not found.
Date Deposited: 31 Mar 2010
Last Modified: 24 May 2010 04:24
URI: http://nal-ir.nal.res.in/id/eprint/3762

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