FIRST LAW OF THERMODYNAMICS 165
dharm
/M-therm/Th4-4.pm5Solution. Flow of fluid = 10 kg/min
Properties of fluid at the inlet :
Pressure, p 1 = 1.5 bar = 1.5 × 10^5 N/m^2
Density, ρ 1 = 26 kg/m^3
Velocity, C 1 = 110 m/s
Internal energy, u 1 = 910 kJ/kg
Properties of the fluid at the exit :
Pressure, p 2 = 5.5 bar = 5.5 × 10^5 N/m^2
Density, ρ 2 = 5.5 kg/m^3
Velocity, C 2 = 190 m/s
Internal energy, u 2 = 710 kJ/kg
Heat rejected by the fluid,
Q = 55 kJ/s
Rise is elevation of fluid = 55 m.
(i) The change in enthalpy,
∆h = ∆u + ∆(pv) ...(i)∆(pv) = pv^221 −pv^11=−=pp 2 × − ×
21
151055
5510
ρρ 26.5
.51.= 1 × 10^5 – 0.0577 × 10^5
= 10^5 × 0.9423 Nm or J = 94.23 kJ
∆u = u 2 – u 1 = (710 – 910) = – 200 kJ/kg
Substituting the value in eqn. (i), we get
∆h = – 200 + 94.23 = – 105.77 kJ/kg. (Ans.)55 mQ12Fluid inFluid outBoundaryFig. 4.44
(ii) The steady flow equation for unit mass flow can be written as
Q = ∆ KE + ∆ PE + ∆ h + Wwhere Q is the heat transfer per kg of fluid