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s344n2d4d5 [400]
3 years ago
14

Nitrogen gas flows through a long, constant-diameter adiabatic pipe. It enters at 100 psia and 120°F and leaves at 50 psia and 7

0°F. Calculate the velocity of the nitrogen at the pipe’s inlet and outlet. The specific heat of nitrogen at the room temperature is cP = 0.248 Btu/lbm·R.
Engineering
2 answers:
inysia [295]3 years ago
7 0

Answer:

Velocity at inlet (V1) = 515.12 ft/s

Velocity at outlet (V2) = 941.43 ft/s

Explanation:

We are given;

Cp = 0.248 Btu/lbm·R.

T1 = 120 °F = 120 + 460 Rankine

= 580 °R

T2 = 70 °F = 70 + 460 R = 530 °R

P1 = 100 psia

P2 = 50 psia

From energy balance equation;

E_in - E_out = ΔEsyst

ΔEsyst = 0.

Thus, E_in = E_out

So,

M'[h1 + V1²/2] = M'[h2 + V2²/2]

M' will cancel out and we have;

[h1 + V1²/2] = [h2 + V2²/2]

V1²/2 - V2²/2 = h2 - h1 - - - - - (eq 1)

Now, h2 - h1 can be expressed as Cp(T2 - T1)

So, V1²/2 - V2²/2 = Cp(T2 - T1)

Also, in ideal gas, we know that;

P1V1/T1 = P2V2/T2

Making V the subject to obtain;

(P1•V1•T2)/(P2•T1) = V2

Putting this for V2 in eq (1), we obtain;

V1²/2 - [(P1•V1•T2)/(P2•T1)]²/2 = Cp(T2 - T1)

Multiply through by 2;

V1² - [(P1•V1•T2)/(P2•T1)]² = 2Cp(T2 - T1)

Lets make V1 the subject;

V1² - V1²[(P1•T2)/(P2•T1)]² = 2Cp(T2 - T1)

V1²[1 - [(P1•T2)/(P2•T1)]²] = 2Cp(T2 - T1)

V1² = 2Cp(T2 - T1)/[1 - [(P1•T2)/(P2•T1)]²]

V1 = √[2•0.248(70 - 120)/[1 - [(100•530)/(50•580)]²]•(25037ft²/lb²/Btu/lbm·R)]

I used the °F for the numerator temperature while I used °R for the denominator temperature so as for the units to cancel out properly.

V1 = √[-24.8)/[1 - 3.34)]•25037]

V1 = √[-24.8)/-2.34)]•25037]

V1 = √[(24.8/2.34)•25037]

V1 =√265349.4017094017

V1 = 515.12 ft/s

Now, to find V2, we recall that,

(P1•V1•T2)/(P2•T1) = V2

We will use the rankine value of temperature.

Thus;

V2 = (100•515.12•530)/(50•580)

= 27301360/29000 = 941.43 ft/s

kari74 [83]3 years ago
5 0

Answer:

V_{1} =515feet/seconds

V_{2} =941.21feet/seconds

Explanation:

We can use balance energy expression.

E_{in} -E_{out} =ΔE_{system}

we have to combine ideal gas and mass balance, so that m_{1} and m_{2} are equal.

m_{1} =m_{2}

therefore

\frac{A_{1} V_{1} }{v_{1} }  =\frac{A_{2} V_{2} }{v_{2} }

make V_{2} the subject of the formula

V_{2} =\frac{A_{1} v_{2} }{A_{2}v_{1}  } (V_{1} )

substitute V_{2} into the energy balance equation

V_{1} =[\frac{2c_{p}(T_{2}-T_{1} )  }{1-(\frac{T_{2}P_{1}  }{T_{1}P_{2}  } )^{2} } ]^{\frac{1}{2} }

now we can substitute the values

V_{1} =[\frac{2*0.248(70-120)}{1-(\frac{530*100}{580*50} )^{2} } ]^{\frac{1}{2} }

V_{1} =515ft/s

Now to find Velocity:

V_{2} =\frac{T_{2} P_{1} }{T_{1}P_{2}  } (V_{1} )

substitute the values

V_{2} =\frac{530*100}{580*50} (515)\\V_{2} =\frac{53000}{29000} (515)\\V_{2} =941.21feet/seconds

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2285kw

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since it is an isentropic process, we can conclude that it is a reversible adiabatic process. Hence the energy must be conserve i.e the total inflow of energy must be equal to the total outflow of energy.

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\\ E_{inflow} = E_{outflow}

Note: from the question we have only one source of inflow and two source of outflow (the exhaust at a pressure of 50kpa and the feedwater at a pressure of 5ookpa). Also the power produce is another source of outgoing energy    \\ E_{inflow} = m_{1} h_{1} .

\\

E_{outflow} = m_{2} h_{2} + m_{3} h_{3} + W_{out}

\\

Where m_{1} h_{1} are the mass flow rate and the enthalpies at the inlet  at a pressure of 3Mpa \\,

m_{2} h_{2} are the mass flow rate and the enthalpies  at the outlet 2 where we have a pressure of 500kpa respectively.\\,

and  m_{3} h_{3}   are the mass flow rate and the enthalpies  at the outlet 3 where we have a pressure of 50kpa respectively.\\,

We can now express write out the required equation by substituting the new expression for the energies \\

m_{1} h_{1} = m_{2} h_{2} + m_{3} h_{3} + W_{out}   \\

from the above equation, the unknown are the enthalpy values and  the mass flow rate. \\

first let us determine the enthalpy values at the inlet and the out let using the Superheated water table.  \\

It is more convenient to start from outlet 3 were we have a temperature 100^{0}C and pressure value of (50kpa or 0.05Mpa ). using double interpolation method  on the superheated water table to determine the enthalpy value with careful calculation we have  \\

h_{3}  = 2682.4 KJ/KG , at this point also from the table the entropy value ,s_{3} value is 7.6953 KJ/Kg.K. \\

Next we determine the enthalphy value at outlet 2. But in this case, we don't have a temperature value, hence we use the entrophy value since the entropy  is constant at all inlet and outlet. \\

So, from the superheated water table again, at a pressure of 500kpa (0.5Mpa) and entropy value of  7.6953 KJ/Kg.K with careful  interpolation we arrive at a enthalpy value of 3206.5KJ/Kg.\\

Finally for inlet one at a pressure of 3Mpa, interpolting with an entropy value of 7.6953KJ/Kg.K  we arrive at enthalpy value of 3851.2KJ/Kg. \\

Now we determine the mass flow rate at each inlet and outlet. since  mass must also be balance, i.e  m_{1} = m_{2} + m_{3} \\

From the question the, the mass flow rate at the inlet m_{1}}  is 2Kg/s \\

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m_{2} = 0.05m_{1} = 0.05 *2kg/s = 0.1kg/s \\

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W_{out} = m_{1} h_{1}-m_{2} h_{2}-m_{3} h_{3}

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\\

W_{out} = 2285.19 kW.

Hence the power produced is 2285kW

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