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kobusy [5.1K]
4 years ago
12

An air-standard dual cycle has a compression ratio of 9.1 and displacement of Vd = 2.2 L. At the beginning of compression, p1 =

95 kPa, and T1 = 290 K. The heat addition is 4.25 kJ, with one quarter added at constant volume and the rest added at constant pressure. Determine: a) each of the unknown temperatures at the various states, in K. b) the net work of the cycle, in kJ. c) the power developed at 3000 cycles per minute, in kW. d) the thermal efficiency. e) the mean effective pressure, in kPa.
Engineering
1 answer:
jok3333 [9.3K]4 years ago
3 0

Answer:

a) T₂ is 701.479 K

T₃ is 1226.05 K

T₄ is 2350.34 K

T₅ is 1260.56 K

b) The net work of the cycle in kJ is 2.28 kJ

c) The power developed is 114.2 kW

d) The thermal efficiency, \eta _{dual} is 53.78%

e) The mean effective pressure is 1038.25 kPa

Explanation:

a) Here we have;

\frac{T_{2}}{T_{1}}=\left (\frac{v_{1}}{v_{2}}  \right )^{\gamma -1} = \left (r  \right )^{\gamma -1} = \left (\frac{p_{2}}{p_{1}}  \right )^{\frac{\gamma -1}{\gamma }}

Where:

p₁ = Initial pressure = 95 kPa

p₂ = Final pressure =

T₁ = Initial temperature = 290 K

T₂ = Final temperature

v₁ = Initial volume

v₂ = Final volume

v_d = Displacement volume =

γ = Ratio of specific heats at constant pressure and constant volume cp/cv = 1.4 for air

r = Compression ratio = 9.1

Total heat added = 4.25 kJ

1/4 × Total heat added = c_v \times (T_3 - T_2)

3/4 × Total heat added = c_p \times (T_4 - T_3)

c_v = Specific heat at constant volume = 0.718×2.821× 10⁻³

c_p = Specific heat at constant pressure = 1.005×2.821× 10⁻³

v₁ - v₂ = 2.2 L

\left \frac{v_{1}}{v_{2}}  \right =r  \right = 9.1

v₁ = v₂·9.1

∴ 9.1·v₂ - v₂ = 2.2 L  = 2.2 × 10⁻³ m³

8.1·v₂ = 2.2 × 10⁻³ m³

v₂ = 2.2 × 10⁻³ m³ ÷ 8.1 = 2.72 × 10⁻⁴ m³

v₁ = v₂×9.1 = 2.72 × 10⁻⁴ m³ × 9.1 = 2.47 × 10⁻³ m³

Plugging in the values, we have;

{T_{2}}= T_{1} \times \left (r  \right )^{\gamma -1}  = 290 \times 9.1^{1.4 - 1} = 701.479 \, K

From;

\left (\frac{p_{2}}{p_{1}}  \right )^{\frac{\gamma -1}{\gamma }}= \left (r  \right )^{\gamma -1} we have;

p_{2} = p_{1}} \times \left (r  \right )^{\gamma } = 95 \times \left (9.1  \right )^{1.4} = 2091.13 \ kPa

1/4×4.25 =  0.718 \times 2.821 \times  10^{-3}\times (T_3 - 701.479)

∴ T₃ = 1226.05 K

Also;

3/4 × Total heat added = c_p \times (T_4 - T_3) gives;

3/4 × 4.25 = 1.005 \times 2.821 \times  10^{-3} \times (T_4 - 1226.05) gives;

T₄ = 2350.34 K

\frac{T_{4}}{T_{5}}=\left (\frac{v_{5}}{v_{4}}  \right )^{\gamma -1} = \left (\frac{r}{\rho }  \right )^{\gamma -1}

\rho = \frac{T_4}{T_3} = \frac{2350.34}{1226.04} = 1.92

T_{5} =  \frac{T_{4}}{\left (\frac{r}{\rho }  \right )^{\gamma -1}}= \frac{2350.34 }{\left (\frac{9.1}{1.92 }  \right )^{1.4-1}} =1260.56 \ K

b) Heat rejected =  c_v \times (T_5 - T_1)

Therefore \ heat \ rejected =  0.718 \times 2.821 \times  10^{-3}\times (1260.56 - 290) = 1.966 kJ

The net work done = Heat added - Heat rejected

∴ The net work done = 4.25 - 1.966 = 2.28 kJ

The net work of the cycle in kJ = 2.28 kJ

c) Power = Work done per each cycle × Number of cycles completed each second

Where we have 3000 cycles per minute, we have 3000/60 = 50 cycles per second

Hence, the power developed = 2.28 kJ/cycle × 50 cycle/second = 114.2 kW

d)

Thermal \ efficiency, \, \eta _{dual} =  \frac{Work \ done}{Heat \ supplied} = \frac{2.28}{4.25} \times 100 = 53.74 \%

The thermal efficiency, \eta _{dual} = 53.78%

e) The mean effective pressure, p_m, is found as follows;

p_m = \frac{W}{v_1 - v_2} =\frac{2.28}{2.2 \times 10^{-3}} = 1038.25 \ kPa

The mean effective pressure = 1038.25 kPa.

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(The diagram of the figure and Free Body Diagram is attached)

<h3>Data given:</h3>

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<h3 /><h3 />

5 0
3 years ago
For some alloy, the yield stress is 345-MPa (50,000-psi) and the elastic modulus (E) is 103-GPa (15x106 psi). What is the maximu
OverLord2011 [107]

The maximum load that may be applied to a specimen with a cross-sectional area of 130 mm² is; 35535 N

<h3>How to find Elastic Modulus?</h3>

We are told that for an alloy, the yield stress is 345-MPa and the elastic modulus (E) is 103-GPa.

Now, we want to find the maximum load that may be applied to a specimen with a cross-sectional area of 130-mm² without plastic deformation. Thus;

We are given the parameters;

Yield Stress; σ = 345 Mpa = 345 * 10⁶ Pa

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Cross sectional Area; A = 130 mm² = 103 * 10⁻⁶ m²

Formula for stress without Plastic deformation is;

σ = F_max/Area

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σ is stress

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Area is Area

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F_max = σ * A

Plugging in the relevant values for stress and area gives us;

F_max = 345 * 10⁶ * 103 * 10⁻⁶

F_max = 35535 N

The maximum load that may be applied to a specimen with a cross-sectional area of 130 mm² is gotten to be 35535 N

Read more about Elastic Modulus at; brainly.com/question/6864866

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2 years ago
Consider a plane composite wall that is composed of two materials of thermal conductivities kA 0.1 W/mK and kB 0.04 W/mK and thi
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Answer:

(a)  761.9 W

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(c) 55.238 °C

(d) see figure

Explanation:

Data

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k_B = 0.04 W/mK

L_A = 0.010 m

L_B = 0.020 m

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T_1 = 200 C

h_1 = 10 W/m^2 K

T_2 = 40 C

h_2 = 20 W/m^2 K

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(a)

The rate of heat transfer is calculated as

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Total flux resistance is

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R_t = (m^2 K)/10 W + (m^2 K)/20 W + 0.010 m (mK)/0.1 W+ 0.020 m (mK)/0.04 W + 0.30 (m^2 K)/W

R_t = 1.05 (m^2 K)/W

From equation 1

Q = 5 m^2 \, \frac{1}{1.05 (m^2 K)/W} \, (200 - 40) K

Q = 761.9 W

(b)

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Q = A \, h_1 \, (T_1 - T_A)

T_A = T_1 - \frac{Q}{A \, h_1}

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Between material B and ambient next to material B heat flux is

Q = A \, h_2 \, (T_B - T_2)

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T_B = \frac{761.9 W}{5 m^2 \, 20 W/m^2 C} + 40 C

T_B = 55.238 C

(d)

See figured attached

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3 years ago
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