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1-D nozzle flow equations using MacCormack method
Hello,
I hope someone can help me out. This may seem like a reasonably simple question. I need to modify MacCormack's method to include the Area and Source terms in order to solve the governing equations for quasi-1-D inviscid nozzle flow: dA*rho/dt + dA*rho*u/dx = 0 dA*rho*u/dt + dA(P + rho*u^2)/dx = P*dA/dx dAE/dt + dA(P + E)u/dx = 0 I would be grateful if somebody could tell me how I should modify the Predictor and Corrector stages to include the additional terms. Thanks very much. |

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