The turbulent flow through a sudden enlargement at subsonic speeds

Kangovi, S and Page, RH (1977) The turbulent flow through a sudden enlargement at subsonic speeds. In: 6th Conference on Australian Hydraulics and Fluid Mechanics, 5-9 Dec 1977, Adelaide, Australia.

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Abstract

The flow through a sudden enlargement was experimentally investigated in the Mach number range of 0.1 to 0.95. Results include variation of base pressure and recovery pressure with reference Mach number. The upstream influence distance and the locations of reattachment and secondary separation points are also reported.

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Aerodynamics;Near wakes;Nozzle flow;Separated flow;Subsonic speed;Turbulent flow;Base pressure;Least squares method; Mach number;Pressure recovery;Reattached flow;Shear layers; Turbulent boundary layers;Upstream;Velocity distribution
Subjects: AERONAUTICS > Aerodynamics
Division/Department: Aerodynamics, Other
Depositing User: M/S ICAST NAL
Date Deposited: 05 Dec 2006
Last Modified: 24 May 2010 09:54
URI: http://nal-ir.nal.res.in/id/eprint/3637

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