AIM:
Aim of this project is to model the Isentropic flow through a quasi 1D subsonic-supersonic nozzle using mathematical equations and solve the equations to simulate a flow.
OBJECTIVES :
The objectives of this project are
To solve the equations that govern the flow through a supersonic nozzle for both conservative and non conservative forms.
To find the differences between them by comparing their solutions.
Steady-state distribution of primitive variables inside the nozzle.
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