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Simora [160]
3 years ago
5

A steady flow adiabatic turbine accepts gas at conditions T1, P1 and discharges at conditions T2 and P2. Assuming ideal gas, det

ermine (per mole of gas) W, Wideal, Wlost and SG for the following. Take Tσ = 300 Κ, Τ1 = 500 Κ, P1 = 6 bar, Τ2 = 371 Κ, P2 = 1.2 bar, and Cp/R = 7/2.
Chemical Engineering (thermodynamics) Please answer as soon as possible.
Engineering
1 answer:
Nimfa-mama [501]3 years ago
5 0

Answer:

W = -3753.8 J

W_{ideal} = - 5163.14 J

W_{lost} = - 1409.34 \ J

S_G = 4.70 \ \ J/K

Explanation:

Given that:

T_1 = 500 \ K \\T_2 = 371 \ K \\T_{\sigma} = 300 \ K\\P_1 = 6 \ bar\\P_2 = 1.2 \ bar\\

\frac{Cp}{R} = \frac{7}{2} \\n = 1

Consider the relation

\frac{Cp}{R} = \frac{7}{2} \\

Cp = \frac{7*R}{2}

Cp = \frac{7*8.314 \ kJ/kmol.K}{2}

Cp = 29.099 \  kJ/kmol.K

Actual work W = ΔH = n Cp (T₂ - T₁)

= 1 × 29.099 (371 - 500)

= -3753.8 J

Change in entropy

ΔS = n[Cp In \frac{T_2}{T_1} - R In \frac{P_2}{P_1}]

ΔS =  1*[29.099 In(\frac{371}{500}) - 8.314 In (\frac{1.2}{6})]

ΔS = 4.6978 J/K

Ideal Work

W_{ideal} = \delta H - T_{\sigma} \delta S

= -3753.8 - 300 ( 4.6978)

= - 5163.14 J

Work lost

W_{lost} = |W_{ideal}-W|

W_{lost} = |-5163.14 -(-3753.8)|

W_{lost} = - 1409.34 \ J

Entropy Generation rate:

S_G = \frac{W_{lost}}{T_{\sigma}}

S_G = \frac{1409.34}{300}

S_G = 4.70 \ \ J/K

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(a) The lower yield point for an iron that has an average grain diameter of 1 x 10-2 mm is 230 MPa. At a grain diameter of 6 x 1
olya-2409 [2.1K]

Answer:

The answer is "4.35 \times 10^{-3}\  mm and 157.5 MPa".

Explanation:

In point A:

The strength of its products with both the grain dimension is linked to this problem. This formula also for grain diameter of 310 MPA is represented as its low yield point  

y =  yo + \frac{k}{\sqrt{x}}

Here y is MPa is low yield point, x is mm grain size, and k becomes proportionality constant.  

Replacing the equation for each condition:  

y = y_o + \frac{k}{\sqrt{(1 \times 10^{-2})}}\\\\\ \ \ \ \ \ \ 230 = yo + 10k\\\\ y = yo + \frac{k}{\sqrt{(6\times 10^{-3})}}\\\\275 = yo + 12.90k

People can get yo = 275 MPa with both equations and k= 15.5 Mpa mm^{\frac{1}{2}}.

To substitute the answer,  

310 = 275 + \frac{(15.5)}{\sqrt{x}}\\\\x = 0.00435 \ mm = 4.35 \times 10^{-3}\  mm

In point b:

The equation is \sigma y = \sigma 0 + k y d^{\frac{1}{2}}

equation is:

75 = \sigma o+4 ky \\\\175 = \sigma o+12 ky\\\\ky = 12.5 MPa (mm)^{\frac{1}{2}} \\\\ \sigma 0 = 25 MPa\\\\d= 8.9 \times 10^{-3}\\\\d^{- \frac{1}{2}} =10.6 mm^{-\frac{1}{2}}\\

by putting the above value in the formula we get the \sigma y value that is= 157.5 MPa

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2 years ago
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Answer:

The strength coefficient is K = 591.87 MPa

Explanation:

We can calculate the strength coefficient using the equation that relates the tensile strength with the strain hardening index given by

S_{ut}=K \left(\cfrac ne \right)^n

where Sut is the tensile strength, K is the strength coefficient we need to find and n is the strain hardening index.

Solving for strength coefficient

From the strain hardening equation we can solve for K

K = \cfrac{S_{ut}}{\left(\cfrac ne \right)^n}

And we can replace values

K = \cfrac{275}{\left(\cfrac {0.4}e \right)^{0.4}}\\K=591.87

Thus we get that the strength coefficient is K = 591.87 MPa

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