Ejector Design Calculation Xls Fix [BEST]

): Determine supersonic velocity at the nozzle exit using the pressure ratio (

Calculate the nozzle throat area: [ A_t = \frac\dotm_1\rho_1 \cdot v_t ] where ( v_t ) is critical (sonic) velocity if the pressure ratio exceeds the critical pressure ratio. ejector design calculation xls

Have questions or found a better correlation? Leave a comment below. ): Determine supersonic velocity at the nozzle exit

The steam expands isentropically from Motive Pressure to Suction Pressure. ejector design calculation xls

High-pressure motive steam expands subsonically and then supersonically across a convergent-divergent (De Laval) nozzle.