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ddd [48]
2 years ago
10

Refrigerant-134a enters a diffuser steadily as saturated vapor at 600 kPa with a velocity of 160 m/s, and it leaves at 700 kPa a

nd 40∘C. The refrigerant is gaining heat at a rate of 2 kJ/s as it passes through the diffuser. If the exit area is 80 percent greater than the inlet area, determine (a) the exit velocity and (b) the mass flow rate of the refrigerant.

Engineering
2 answers:
Zina [86]2 years ago
4 0

Answer:

a) V_2 = 82.1 m/s

b) m = 0.298 Kg/s

Explanation:

from A-11 to A-13 we have the following data

P_1 = 600 kpa

V_1 = 0.033925 m^3/kg

h_1 = 262.52 kJ/kg

P_2 = 700 kpa

V_2 = 0.0313 m^3/kg

T_2 = 40°C = 313K

h_2 = 278.66 kJ/kg

Now, from the conversation of mass,

A_2*V_2/u_2 = A_1*V_1/u_1

V_2 = A_1/A_2*u_2/u_1*V_1

V_2 = A_1/1.8*A_1 * 0.0313 /0.033925*160

V_2 = 82.1 m/s

now from the energy balance equation

E_in = E_out

Q_in + m(h_1 + V_1^2/2) =  m(h_2 + V_2^2/2)

m = 0.298 Kg/s

grin007 [14]2 years ago
4 0

Answer:

A) V2 = 82.1 m/s

B) m' = 0.298 kg/s

Explanation:

A) From the tables attached,

At P1 = 600 KPa, we have specific volume and specific enthalpy as;

v1 = 0.033925 m³/kg

And h1 = 262.52 Kj/kg or 262520 J/kg

Also at P2 = 700 KPa, and T2 = 40°C = 313K, we have specific volume and specific enthalpy as ;

v2 = 0.03133 m³/kg and h2 = 278.66 Kj/kg or 278660 J/kg

From conservation of mass, we know that;

A1V1/v1 = A2V2/v2

So, making V2 the subject, we have;

(A1V1v2)/(v1A2) = V2

Now, from the question, the exit area (A2) is 80% greater than the inlet Area (A1). Thus, A2 = A1 + 0.8A1 = 1.8A1

So,

(A1V1v2)/(v1 x 1.8 xA1) = V2

So, A1 will cancel out to give;

(V1v2)/(v1 x 1.8) = V2

Plugging in relevant values;

(160 x 0.0313)/(0.033925 x 1.8) = 82.1 m/s

B) From energy balance, we know that;

E'in = E'out

Thus,

Q'in + m'(h1 + (v1²/2)) = m'(h2 + (v2²/2))

From the question, Q'in = 2kj = 2000J

Thus;

2000 + m'(262520 + (160²/2)) = m'(278660 + (82.1²/2))

So,

2000 + 275320m' = 282030 m'

m'(282030 - 275320) = 2000

m' = 2000/6710 = 0.298 kg/s

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Answer:

Yes, the flow is turbulent.

Explanation:

Reynolds number gives the nature of flow. If he Reynolds number is less than 2000 then the flow is laminar else turbulent.

Given:

Diameter of pipe is 10mm.

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Step1

Expression for Reynolds number is given as follows:

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Substitute the values in the above equation as follows:

Re=\frac{vd}{\nu}

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Thus, the Reynolds number is 64226.07579. This is greater than 2000.

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Radioactive wastes are temporarily stored in a spherical container, the center of which is buried a distance of 10 m below the e
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prohojiy [21]

Answer:

i) S–N plot is attached

ii) fatigue strength = 100 MPa

iii) fatigue life = 5.62 x 10^(5) cycles

Explanation:

i) I have attached the S–N plot (stress amplitude versus logarithm of cycles to failure)

ii) The question says we should find the fatigue strength at 4 × 10^(6) cycles.

So let's find the log of this and trace it on the graph attached.

Log(4 × 10^(6)) = 6.6

From the graph attached, at log of cycle value of 6.6, the fatigue strength is approximately 100 MPa

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8 0
2 years ago
The emissivity of galvanized steel sheet, a common roofing material, is ε = 0.13 at temperatures around 300 K, while its absorpt
Step2247 [10]

Answer:

759.99W/m²

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Question: If the temperature of the sheet is 77C,what is the incident solar radiation on aday with Tinf= Tsurr= 16°C?

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Energy Equation of the Gas

αs * Gs * A + h * A * (T inf - Tg) + εσA (Tsurr⁴- Tg⁴) = 0

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h = 7W/m²K⁴

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A cancels out, so we are left with

0.65 * Gs = - 7 * (288.15 - 350.15) - 0.13 * 5.67 * 10^-8 * (288.15⁴ - 350.15⁴)

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0.65Gs = 434 + 0.7372 * 81.37940481697

0.65Gs = 493.992897231070284

Gs = 493.992897231070284/0.65

Gs = 759.9890726631850

Gs = 759.99W/m² ------- Approximated

3 0
2 years ago
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