Week 2 - Converging diverging nozzle

Converging diverging nozzle

1 Create the geometry using design software for the above-mentioned dimensions.

2 And import the geometry to Ansys-Spaceclaim as shown below

Meshing

Simulations

Start the fluent simulation setup using 2D.
Apply the boundary conditions for To the suitable boundaries as shown below.
And run the calculation,

Variations of Mach number

Pressure and velocity at outlet

conclusion

Hence, we plotted the various factors for the nozzle domain.
And, also we have seen the effects on mach number on changing the area of the nozzles.
Also, we got the same solutions from the three different methods.