Steam with a flow rate of 1360 kg/h enters an adiabatic nozzle (adiabatic, Q=0) at 1378
kPa, specific volume of 0.147 m3
/kg, and specific internal energy of 2510 kJ/kg. The exit
conditions are 137.8 kPa, 1.099 m3
/kg specific volume, and 2263 kJ/kg of specific internal
energy. Find the exit velocity.
Solution;
For an adiabatic nozzle;
W=0
Q=0
Given;
"\\dot{m}=1360kg\/h=0.3778kg\/s"
"P_1=1378kPa"
"v=0.147m^3\/kg"
"u_1=2510kJ\/kg"
"P_2=137.8kPa"
"v_2=1.099m^3\/kg"
"u_2=2263kJ\/kg"
"V_1=3.05m\/s"
Energy balance equation;
"h_1+\\frac{v_1^2}{2000}=h_2+\\frac{v_2^2}{2000}"
But h=u+PV
"u_1+P_1v_1+\\frac{V_1^2}{2000}=u_2+P_1v_1+\\frac{V_2^2}{2000}"
By direct substitution;
"2510+1378\u00d70.147+\\frac{3.05^2}{2000}=2263+137.8\u00d71.099+\\frac{V_2^2}{2000}"
"V_2^2=621409.3025"
"V_2=788.3m\/s"
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