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Project Description

CFD simulation of flow separation in supersonic nozzle with ANSYS Fluent software

Supersonic flow analysis in nozzles regarding the numerous uses of this series of fluid interfaces in various topics of fluid mechanics, has become one of the most popular branches of mechanical science.

The use of these nozzles, especially in the air industry, manufacture of missiles, planes, and spacecraft, has led to many studies in this field.

The nature of the fluid behavior in the nozzles, which is based on the change in fluid density due to extreme changes in velocity and pressure over a small distance, has led to different methods being proposed to examine it.

In the meantime, Density-Based solvers provide the best results in the analysis.

In this analysis, we tried to simulate and analyze the separation of flow in supersonic nozzles using a Density-Based solver using ANSYS Fluent software.

For a constant area ratio, the ratio of the output area to the throttle, the calculations are carried out in a range of nozzle pressures ratio. This review is compared with experimental results.

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Project Details

TITLE: CFD simulation of flow separation in supersonic nozzle with ANSYS Fluent software

PROJECT TYPE: Mechanical, Supersonic Flow

TIME: 49 days



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