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mestny [16]
4 years ago
11

Log mean temperature difference, FT applied to heat exchangers. Problem 4.9-2, p351. Oil flowing at the rate of 5.04 kg/s (Cpm =

2.09 kJ/kg.K) is cooled in a 1-2 heat exchanger from 366.5 K to 344.3 K by 2.02 kg/s of water entering at 283.2 K. The overall heat transfer coefficient U0, is 340 W/m^2 .K. Calculate the area required. (Hint: a heat balance must first be made to determine the outlet water temperature.)
Engineering
1 answer:
bazaltina [42]4 years ago
5 0

Answer:

the Area required is 12m2

Explanation:

A heat exchanger is a mechanical device used to transfer heat from one fluid to another by heating or cooling one of the fluids with the help of the other. They are of different types which include;

Shell and Tube heat exchangers, that categorically involves large number of small tubes embedded within a cylindrical shell. It may be

1 shell 1 tube pass (1-1 exchanger) which means the heat enters through one end and travels on a straight line to exit the other end.

1 shell multi-tube pass (1-2,1-4,1-6,1-8 etc exchangers) meaning the heat enters through one end, and travels in a directed path to exit a different end.

To calculate the quantity of heat exchanged for both cases, we use the same formula

Q=UA∆Tlm

Where Q= Rate of Quantity of heat exchanged

U= Heat transfer coefficient

A=Area of tube

Tlm= Logarithm mean temperature difference which signifies the average logarithm of the difference in temperature between the hot region and the cold region of both ends of the pipe exchanger.

The major difference is that,

For 1-1 exchanger, Tlm=Tm= [(Thi-Tco)-(Tho-Tci)]/ln[(Thi-Tco)/(Tho-Tci)]

But

For 1-2, 1-4, 1-6 etc exchangers, Tlm=Tm×F

Where F is called the correction factor, and it is the point on the graph (of correction factor (F) plotted against Log mean temperature difference (Tlm) for cross-flow exchangers) where the Y value and Z value intercepts.

The Y and Z values can be calculated using the Formulas below

Y=[(Tco-Tci)/(Thi-Tci)] and Z=[(Thi-Tho)/(Tco-Tci)]

For the question above, to find the Area of tube, we need to calculate the rate of quantity of heat exchanged (Q), then use the value to find the outlet temperature of cold fluid (Tco), then find the Log mean temperature difference which will require F,Y,Z and Tm, then use the results gotten to compute the Area.

Given;

Mass flow rate of hot fluid (oil), Mh=5.04kg/s

Specific heat of hot fluid, Cph=2.09kj/kg.k

Inlet temperature of hot fluid, Thi=366.5K

Mass flow rate of cold fluid (water), Mc=2.02kg/s

Specific heat of cold fluid, Cpc=4.186kj/kg.k

Inlet temperature of cold fluid, Tci=283.2K

Outlet temperature of hot fluid, Tho=344.3k

Outlet temperature of cold fluid = Tco

Overall heat transfer coefficient, U= 340W/m2.k

Area of tube =A

First we have to find the quantity of heat exchanged (Q). We use,

Qh=∆Hh=MhCph(Tho-Thi)

=5.04×2.09 × (344.3-366.5)

=-233.85kj/s

The quantity of heat lost by the hot fluid Qh is equal to the quantity of heat gained by the cold Fluid Qc.

Therefore;

Qh=Qc

Qc=233.85kj/s

To calculate Tco, we use

Qc=∆Hc=McCpc(Tco-Tci)

233.85=2.02×4.186×(Tco-283.2)

233.85=8.45572Tco-2394.66

Tco=(233.85+2394.66)/8.45572=310.86k

Next, we use the formula Q=UA∆Tlm to get our A, but for 1-2 exchanger,

Tlm=Tm×F

So we find F using Y and Z values

Y=(Tco-Tci)/(Thi-Tci)=(310.86-283.2)/(366.5-283.2)=0.3321

Z=(Thi-Tho)/(Tco-Tci)=(366.5-344.3)/(310.86-283.2)=0.8026

At point Y=0.3321 and point Z=0.8026, we have an intercept of F=0.975

Also,

Tm=[(Thi-Tco)-(Tho-Tci)]/Ln[(Thi-Tco)/(Tho-Tci)]

=[(366.5-310.86)-(344.3-283.2)]/ln[(366.5-310.86)/(344.3-283.2)]

=(-5.46)/(-0.0936)=58.33k

∆Tlm=Tm×F

=58.33×0.975

=56.872k

Now to get A, we input all calculated values into our general formula;

Q=233.85Kj= (233.85×1000)j

Q=UA∆Tlm

233.85×1000=340×A×56.872

A=(233.85×1000)/(340×56.872)=12m2

Therefore, the Area required is 12m2.

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A converging-diverging nozzle has an area ratio of 5.9. (1) Determine the (P0/Pt) values corresponding to the 1st, 2nd, and 3rd
nata0808 [166]

Answer:

Check the explanation

Explanation:

The Total pressure is the overall of fixed or static pressure p, the dynamic pressure q, as well as gravitational head. Total pressure can also be referred to as the measure of the overall energy of the airstream, and is the same to static pressure plus velocity pressure.

kindly check the step by step solution in the attached image below to Determine the (P0/Pt) values corresponding to the 1st, 2nd, and 3rd critical points.

5 0
3 years ago
A square-thread power screw is used to raise or lower the basketball board in a gym, the weight of which is W = 100kg. See the f
KIM [24]

Answer:

power = 49.95 W

and it is self locking screw

Explanation:

given data

weight W = 100 kg = 1000 N

diameter d = 20mm

pitch p = 2mm

friction coefficient of steel f = 0.1

Gravity constant is g = 10 N/kg

solution

we know T is

T = w tan(α + φ ) \frac{dm}{2}     ...................1

here dm is = do - 0.5 P

dm = 20 - 1

dm = 19 mm

and

tan(α) = \frac{L}{\pi dm}      ...............2

here lead L = n × p

so tan(α) = \frac{2\times 2}{\pi 19}

α = 3.83°  

and

f = 0.1

so tanφ = 0.1

so that φ = 5.71°

and  now we will put all value in equation 1 we get

T = 1000 × tan(3.83 + 5.71 ) \frac{19\times 10^{-3}}{2}  

T = 1.59 Nm

so

power = \frac{2\pi N \ T }{60}     .................3

put here value

power = \frac{2\pi \times 300\times 1.59}{60}

power = 49.95 W

and

as φ > α

so it is self locking screw

 

8 0
3 years ago
A transformer winding contains 900 turns of wire which creates 400 ohms of primary importance how many terms of the same size wi
Eduardwww [97]

Answer: 255

255 turns are required to create 25 ohms of  secondary impedance.

Explanation:

Given that,

Number of turns in primary wire N₁ = 900

impedance on Primary wire Z₁ = 400 ohms

Number of turns in Secondary wire N₂ = ?

impedance on Secondary wire Z₂ = 25 ohms

we know that, the relationship between turn and impedance is

Zp / Zs = ( Np / Ns )²

(Primary impedance / secondary impedance) = Number of turns in primary wire / Number of turns in secondary wire)²

there fore

Z₁ / Z₂ = ( N₁ / N₂ )²

Now we substitute

( 400 / 25 ) = ( 900 / N₂ )²

400 / 25 = 900² / N₂²

we cross multiple to get our N₂

400 × N₂² =  900² × 25

N₂² = ( 900² × 25 ) / 400

N₂² = ( 810000 × 25 ) / 400

N₂² = 20250000 / 400

N₂² = 50625

N₂ = √50625

N₂ = 225

Therefore 255 turns are required to create 25 ohms of  secondary impedance.

4 0
3 years ago
A sand has a natural water content of 5% and bulk unit weight of 18.0 kN/m3. The void ratios corresponding to the densest and lo
Zinaida [17]

Answer:

Relative density = 0.545

Degree of saturation = 24.77%

Explanation:

Data provided in the question:

Water content, w = 5%

Bulk unit weight = 18.0 kN/m³

Void ratio in the densest state, e_{min} = 0.51

Void ratio in the loosest state, e_{max} = 0.87

Now,

Dry density, \gamma_d=\frac{\gamma_t}{1+w}

=\frac{18}{1+0.05}

= 17.14 kN/m³

Also,

\gamma_d=\frac{G\gamma_w}{1+e}

here, G = Specific gravity = 2.7 for sand

17.14=\frac{2.7\times9.81}{1+e}

or

e = 0.545

Relative density = \frac{e_{max}-e}{e_{max}-e_{min}}

= \frac{0.87-0.545}{0.87-0.51}

= 0.902

Also,

Se = wG

here,

S is the degree of saturation

therefore,

S(0.545) = (0.05)()2.7

or

S = 0.2477

or

S = 0.2477 × 100% = 24.77%

7 0
3 years ago
PLS HELP!!!
Advocard [28]

Answer:

I would say C

Explanation:

let me know if im right

3 0
2 years ago
Read 2 more answers
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