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Abstract
The choking phenomenon of a convergent nozzle flow has been experimentally investigated using four nozzles with the same diameter but different boundary layer thickness at the exit of the nozzle. It is observed that the pressure ratio across the nozzle when the flow is just choked depends on the boundary layer thickness at the nozzle exit, and both the choking pressure ratio and the choked mass flow rate decrease with increasing boundary layer thickness. The main flow at the exit of the nozzle when the flow is choked is supersonic, and the Mach number increases with increasing boundary layer thickness.
Journal
- Transactions of the Japan Society of Mechanical Engineers. B [List of Volumes]
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Transactions of the Japan Society of Mechanical Engineers. B 75(752), 724-729, 2009-04-25 [Table of Contents]
The Japan Society of Mechanical Engineers