Thermodynamics flow control?

In summary: It assumes constant specific heats, but that's usually good enough, as long as you're not too far beyond the critical.In summary, the Wivenhoe hydroelectric power station requires two pumps, each consuming 250 MW of power at 98% efficiency, to elevate water from Wivenhoe Dam to Splityard Creek Dam. The water is pumped approximately 70 m and released at 1 atm through a pipe of 20 m diameter. At full power, Splityard Creek Dam can be filled from empty to its capacity of 28,700 ML in 14 hours. The supplied water is stationary at 4 atm and 10°C, with no
  • #1
campblor
6
0
I have this problem and have been pulling what's left of my hair out:
The Wivenhoe hydroelectric power station requires water to be pumped from Wivenhoe Dam to
Splityard Creek Dam, using two pumps (each consuming 250 MW of power at 98% efficiency) to
elevate the water approximately 70 m. At full power, Splityard Creek Dam can be filled from empty
to its capacity of 28 700 ML in 14 hours. The water being supplied is stationary at 4 atm and 10°C; it
is released at 1 atm through a pipe of 20 m diameter.
Assume that there will be no net heat transfer to the water. What is the maximum
temperature at which the water will exit?

Values that I'm using
State 1:
P1 = 405.3kPa T1 = 10C; h1=42.022kj/kg
KE1 = 0 ; PE1 = 0

State 2:
P2 = 101.325kPa

Ive got a volume flow rate of 569.4x103 L/s hence a mass flow rate of 569.4x103 kg/s

and doing some algebra from Mass flow rate = (density)*(Velocity)*(Cross-sectional Area) v = 1.8m/s
and A = 314.16m2
Win = 2x(250MW x 0.98) = 490,000kWFrom the 1st Law using
Win+m(h1+P1/p)=m(h2+P2/p+V^2/2+gz2).

my idea is to use the 1st law to find h2 and use that with the Pressure at state 2 get the temp.

but it give me a value of -643.71kJ/kg

There must be something I'm missing or completely off track..

any asssistance would be greatly appreciated
 
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  • #2
The term P/p is included in the definition of enthalpy in the first law, as it is defined by h = u + P/p. So yeah, your formula for the first law should not include the P/p terms.

EDIT: I didn't realize you were using h for internal energy instead of enthalpy; In that case, your arithmetic is probably off.
 
Last edited:
  • #3
It looks like your approach is correct, so let's see your arithmetic.

Chet
 
  • #4
Net heat transfer to the water is 0; delta Q = 0

-Wout = 0; Win = 2x(250MW x 0.98) = 490000kW

m = 569444kg/s

h1 = hf@10C = 42.022kJ/kg; h2=?

ke2 = ½ v^2 = 1/2x(1.8m/s)^2 = 1.6m/s^2; ke1 = 0

pe2 = gz2 = 9.81m/s^2 x 70m = 686.7; pe1 = 0

Qin – Qout + Win – Wout = m(h2 – h1 + ke2 – ke1 + pe2 – pe1)

Win = m(h2 – h1 + ke2 + pe2)

Win/m = h2 – h1 + ke2 + pe2

h2 = (Win/m) +h1 – ke2 – pe2

h2 = (490000kJ/s / 569444kg/s) + 42.022kJ/kg - 1.6m/s^2 – 687.7m/s^2

h2 = -646 kJ/kg
 
  • #5
campblor said:
h2 = (490000kJ/s / 569444kg/s) + 42.022kJ/kg - 1.6m/s^2 – 687.7m/s^2

2 things:
- Again, the value of 42.022 kJ/kg is only the internal energy, not the enthalpy, which is what you need (although the error is quite small)
- Your equation is not dimensionally consistent, you are subtracting J/kg from kJ/kg. This is the primary reason its failing.
 
  • #6
I'm getting the 42.022kJ/kg from the Sat. liquid hf@10C from table A-4

I'm completely lost with your second point sorry - I think I've been looking this for so long that my pea brain had turned to pea mush
 

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  • #7
or was i meant to have the ke2 & pe2 both be multiplied by (1kJ/kg / 1000m^2/s^2)
 
  • #8
The enthalpy h1 should be about 42.4 kJ/kg for water at p = 405.3 kPa and T = 10C. You can either look it up for water at 10C and 405.3 kPa, or calculate it from the internal energy as:

h1 = u1 + P1/p1 = 42 [kJ/kg] + 405.3 [kPa] /1000 [kg/m^3] = 42.4 kJ/kg (this is just an approximation, but its consistent with an online calculator).

For my second point, its very important that you make sure the units match:

1 km + 1 m is not 2 km, but 1.001 km. Similarly:

campblor said:
h2 = (490000kJ/s / 569444kg/s) + 42.022kJ/kg - 1.6m/s^2 – 687.7m/s^2

The first two terms are in kJ/kg, but the last 2 are in J/kg. Therefore, you should divide the last 2 terms by 1000 to convert them to kJ/kg:

h2 = (490000kJ/s / 569444kg/s) + 42.4kJ/kg - (1.6/1000)[kJ/kg] – (687.7/1000)[kJ/kg]
 
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  • #9
Thanks mate, I really appreciate that!:smile:

That definitely makes sense now. Its the little things that make a big difference!:cool:
 
  • #10
Also, I think you're using the wrong table for water. You are using the table for saturated water. In that condition, the thermodynamic properties of water are determined by either T and P, T and P are dependent in that state. However, the state the water is in here is not saturated water, so you have to use the correct table.
 
  • #11
Kyouran said:
Also, I think you're using the wrong table for water. You are using the table for saturated water. In that condition, the thermodynamic properties of water are determined by either T and P, T and P are dependent in that state. However, the state the water is in here is not saturated water, so you have to use the correct table.

Thanks,I'll go back and hit the books harder to get my basics up to scratch

I'm studying Thermodynamics by correspondence - its a difficult subject as it is, but without the face to face interaction it makes it twice as hard.

Thanks again for taking your time to help me out
 
  • #12
Kyouran said:
The term P/p is included in the definition of enthalpy in the first law, as it is defined by h = u + P/p. So yeah, your formula for the first law should not include the P/p terms.

EDIT: I didn't realize you were using h for internal energy instead of enthalpy; In that case, your arithmetic is probably off.
Kyouran,
Thanks for pointing this out. I missed that in my post # 3.

Chet
 
  • #13
Kyouran said:
Also, I think you're using the wrong table for water. You are using the table for saturated water. In that condition, the thermodynamic properties of water are determined by either T and P, T and P are dependent in that state. However, the state the water is in here is not saturated water, so you have to use the correct table.
The steam tables I have only give values for saturation and superheating. However, the relationship you gave in post #8 can be accurately used, as long as you're not too close to the critical point.

Chet
 
  • #14
This problem could have been done so much more easily, without the use of the steam tables, simply by writing:
$$h_2-h_1=C_p(T_2-T_1)+\frac{(P_2-P_1)}{ρ}$$

Chet
 

What is thermodynamics flow control?

Thermodynamics flow control is a branch of science that studies the principles of energy and its transformation in various systems, particularly in relation to the flow of heat and work.

What is the role of thermodynamics flow control in engineering?

Thermodynamics flow control plays a crucial role in engineering as it helps in designing and optimizing systems that involve energy transfer, such as engines, power plants, and refrigeration systems.

What are the laws of thermodynamics flow control?

The first law states that energy cannot be created or destroyed, only transferred or converted from one form to another. The second law states that the total entropy of a closed system will always increase over time. The third law states that absolute zero temperature cannot be reached through a finite number of steps.

What are the different types of energy transfer in thermodynamics flow control?

There are three main types of energy transfer in thermodynamics flow control: conduction, convection, and radiation. Conduction is the transfer of heat through a solid material. Convection is the transfer of heat through a fluid or gas. Radiation is the transfer of heat through electromagnetic waves.

How is thermodynamics flow control applied in real-life situations?

Thermodynamics flow control is applied in various real-life situations, such as in the design of engines for cars and airplanes, in the production of electricity in power plants, and in the development of refrigeration and air conditioning systems. It also plays a role in understanding weather patterns and climate change.

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