Ejector Design Calculation Xls Fixed _top_ [ DIRECT ]

Use the isentropic expansion equation to find the Mach number. For steam, the nozzle is typically convergent-divergent (C-D) to achieve supersonic speeds.

Integrate a check formula for the Critical Pressure Ratio ( Critical Ratio Formula: = (2 / (k + 1)) ^ (k / (k - 1)) ejector design calculation xls fixed