Which equation is the CORRECT representation of the steady flow energy equation for a nozzle?

1
\({h_1} + \frac{{C_1^2}}{2} = {h_2} + \frac{{C_2^2}}{2}\)
2
\({h_1} + \frac{{{C_1}}}{2} = {h_2} + \frac{{{C_2}}}{2}\)
3
\({h_1} - \frac{{C_1^2}}{2} = {h_2} - \frac{{C_2^2}}{2}\)
4
\({h_1} - \frac{{{C_1}}}{2} = {h_2} - \frac{{{C_2}}}{2}\)

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