Kangovi, S and Page, RH (1978) Subsonic turbulent flow past a downstream facing annular step. In: Winter Annual Meeting on American Society of Mechanical Engineers, 10-15 Dec 1978, California, USA.Full text not available from this repository.
The flow past a downstream facing annular step was experimentally investigated in the Mach number range of 0.1 to 0.95. The approaching flow was steady and uniform. The boundary layer ahead of the step was turbulent. The upstream influence of the step and the variation of base pressure and recovery pressure with the reference Mach number are described. Results of hot-wire measurements in the shear layer and the locations of reattachment and secondary separation points are also reported.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||Annuli;Near wakes;Pipe flow;Separated flow;Subsonic flow; Turbulent flow;Base pressure;Hot wire flow meters;Pressure distribution;Reattached flow;Shear layers;Wind tunnel tests|
|Subjects:||AERONAUTICS > Aerodynamics|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||05 Dec 2006|
|Last Modified:||24 May 2010 09:53|
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