The energy equation can be reduced to the following form:
\[ \frac{P_1 - P_2}{\rho} = \frac{v_2^2}{2} + K_{entrance} \times \frac{v_2^2}{2} \]
where $P_1$ and $P_2$ are the pressures at the beginning and end of the diffuser, $v_2$ is the velocity at the end of the
Show more…