Tank is evacuated and send air into the tank by supply line through a valve.
Supply line condition :
Initial temperature T1 = 100 F
Pressure P1 = 50 Psia
As we know that tank is evacuated then having no initial pressure and temperature. All inlet enthalpy of air is get converted into internal energy of air inside the tank.
1. Adiabatic operation Q = 0
2. Negligible kinetic and potential energy.
3. No boundaey work done and no shaft work.
For supply line it having flow so we use enthalpy and evacuated tank it having constant volume so we use internal energy.
Mass of the air in supply line and after getting all air inside the tank is same.
Enthalpy of air inlet = internal energy of air inside tank after getting air into the tank
H1 = U2
CpT1 = CvT2
Cp - heat capacity at constant pressure
Cv - heat capacity at constant volume
Gamma heat capacity ratio Y = Cp/Cv = 1.4
Gas constant,
R = 10.73 ft3. psia/lbmol*R
T2 = (Cp/Cv) * T1 = 1.4*100 = 140 F
Conversion of temperature : F to R
F + 459.67 = R
At 140F
R = 140+459.67 = 599.67 R
T2 = 599.67 R
Given tank volume V = 100 ft3
After getting air, volume of air V = 10 ft3, Pressure remains same because there is tank evacuated initially P = 50 psia and T2 = 599.67 R
By using ideal gas equation
PV = nRT
n = PV/RT
n = 50 psia * 10 ft3/(10.73ft3.psia/lbmol*R)*599.67R
n = 0.0777 lbmol
Molecular weight of air M = 29 lbm/lbmol
Mass of air =0.0777lbmol * 29 lbm/lbmol = 2.253 lbm
amount of air that got the air, m = 2.253 lbm.
Yes this process happen. All flow energy get used to increase the internal energy of air after getting all air.
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