A convergent nozzle with exit diameter of 2 cm has an air inlet flow of 20°C, 101 kPa (stagnation conditions). The nozzle has an isentropic efficiency of 95% and the pressure drop is measured to 50 cm water column. Find the mass flow rate assuming compressible adiabatic flow. Repeat calculation for incompressible flow.
Convert ΔP to kPa:
Assume inlet V _{ i }=0 \quad P _{ e }= P _0-\Delta P =101-4.903=96.097 \,kPa
= 4.1545 kJ/kg = 4254.5 J/kg \Rightarrow \mathbf{V} _{ e }=91.15 \,m / s