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Varvara68 [4.7K]
3 years ago
14

Water at 20 bar and 400 C enters a turbine operating at steady state and exits at 1.5 bar. Stray heat transfer and kinetic and p

otential energy effects are negligible. A hard-to-read data sheet indicates that the quality, x, at the turbine exit is 98%. What is the value of entropy at the turbine inlet in kJ/kg-K?
Engineering
1 answer:
kherson [118]3 years ago
4 0

Answer:

s_1=7.1292\frac{kJ}{kg*K}, nevertheless, the outlet quality is not possible due to negative entropy generation.

Explanation:

Hello,

In this case, with the given conditions, it is possible to extract the entropy at the turbine inlet from the steam overheated tables at 20 bar and 400 °C, realizing that 20 bar equals 2 MPa. In such a way, the entropy at those conditions is:

s_1=7.1292\frac{kJ}{kg*K}

Moreover, we should prove that the 98% quality is possible in terms of the entropy generation which MUST be positive based on the entropy balance:

s_{gen}=s_2-s_1

Thus, we also compute the entropy at the outlet, looking for liquid-vapor water at 1.5 bar with the given quality:

s_2=1.3548\frac{kJ}{kg*K}+0.98*5.9187\frac{kJ}{kg*K}\\s_2=7.155\frac{kJ}{kg*K}

Hence the entropy generation turns out:

s_{gen}=s_2-s_1=7.155-7.1292=-0.0259\frac{kJ}{kg*K}

Finally, such value means that the outlet quality is not thermodynamically possible.

Regards.

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Consider a modification of the air-standard Otto cycle in which the isentropic compression and expansion processes are each repl
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Answer:

The answers to the question are

(1) Process 1 to 2

W = 295.16 kJ/kg

Q = -73.79 kJ/kg

(2) Process 2 to 3

W = 0

Q = 1135.376 kJ/kg

(3) Process 3 to 4

W = -1049.835 kJ/kg

Q = 262.459 kJ/kg

(4) Process 4 to 3

W=0

Q = -569.09 kJ/kg

(b) The thermal efficiency = 49.9 %

(c) The mean effective pressure is 9.44 bar

Explanation:

(a) Volume compression ratio \frac{v_1}{v_2}  = 10

Initial pressure p₁ = 1 bar

Initial temperature, T₁ = 310 K

cp = 1.005 kJ/kg⋅K

Temperature T₃ = 2200 K from the isentropic chart of the Otto cycle

For a polytropic process we have

\frac{p_1}{p_2}  = (\frac{v_2}{v_1} )^n Therefore p₂ = p₁ ÷ (\frac{v_2}{v_1} )^n = (1 bar) ÷ (\frac{1}{10} )^{1.3} = 19.953 bar

Similarly for a polytropic process we have

\frac{T_1}{T_2}  = (\frac{v_2}{v_1} )^{n-1} or T₂ = T₁ ÷ (\frac{v_2}{v_1} )^{n-1} = \frac{310}{0.1^{0.3}} = 618.531 K

The molar mass of air is 28.9628 g/mol.

Therefore R = \frac{8.3145}{28.9628} = 0.287 kJ/kg⋅K

cp = 1.005 kJ/kg⋅K Therefore cv = cp - R =  1.005- 0.287 = 0.718 kJ/kg⋅K

1). For process 1 to 2 which is polytropic process we have

W = \frac{R(T_2-T_1)}{n-1} = \frac{0.287(618.531-310)}{1.3 - 1}= 295.16 kJ/kg

Q =(\frac{n-\gamma}{\gamma - 1} )W = (\frac{1.3-1.4}{1.4-1} ) 295.16 kJ/kg = -73.79 kJ/kg

W = 295.16 kJ/kg

Q = -73.79 kJ/kg

2). For process 2 to 3 which is reversible constant volume heating we have

W = 0 and Q = cv×(T₃ - T₂) = 0.718× (2200-618.531) = 1135.376 kJ/kg

W = 0

Q = 1135.376 kJ/kg

3). For process 3 to 4 which is polytropic process we have

W = \frac{R(T_4-T_3)}{n-1} = Where T₄ is given by  \frac{T_4}{T_3}  = (\frac{v_3}{v_4} )^{n-1} or T₄ = T₃ ×0.1^{0.3}

= 2200 ×0.1^{0.3}  T₄ = 1102.611 K

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and Q = 262.459 kJ/kg

W = -1049.835 kJ/kg

Q = 262.459 kJ/kg

4). For process 4 to 1 which is reversible constant volume cooling we have

W = 0 and Q = cv×(T₁ - T₄) = 0.718×(310 - 1102.611) = -569.09 kJ/kg

W=0

Q = -569.09 kJ/kg

(b) The thermal efficiency is given by

\eta = 1-\frac{T_4-T_1}{T_3-T_2} =1-\frac{1102.611-310}{2200-618.531} = 0.499 or 49.9 % Efficient

(c) The mean effective pressure is given by

p_{m}  = \frac{p_1r[(r^{n-1}-1)(r_p-1)]}{ (n-1)(r-1)}  where r = compression ratio and r_p = \frac{p_3}{p_2}

However p₃ = \frac{p_2T_3}{T_2} =\frac{(19.953)(2200)}{618.531} =70.97 atm

r_p = \frac{p_3}{p_2} = \frac{70.97}{19.953}  = 3.56

Therefore p_m =\frac{1*10*[(10^{0.3}-1)(3.56-1)]}{0.3*9} = 9.44 bar

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Explanation:

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