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

A

$$h_1 + \frac{c_1^2}{2} = h_2 + \frac{c_2^2}{2}$$

B

$$h_1 + \frac{c_1}{2} = h_2 + \frac{c_2}{2}$$

C

$$h_1 - \frac{c_1^2}{2} = h_2 - \frac{c_2^2}{2}$$

D

$$h_1 - \frac{c_1}{2} = h_2 - \frac{c_2}{2}$$