Project

1D Super-sonic nozzle flow simulation using Macormack Method

Objective: Non Conservative form of Equation in terms of Normalised parameters: Continuity Equation `(delrho)/(delt)=-rho*(delV)/(delx)-rho*V*(dellnA)/(delx)-V*(delrho)/(delx)` Momentum Equation `(delV)/(delt)=-V*(delV)/(delx)-1/(gamma)*((delT)/(delx)+T/rho*(delrho)/(delx))` Energy Equation `(delT)/(delt)=-V*(delT)/(delx)-(gamma-1)*T*((delV)/(delx)+V*(dellnA)/(delx))`…

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