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vichka [17]
3 years ago
10

A reversible compression of 1 mol of an ideal gas in a piston/cylinder device results in a pressure increase from 1 bar to P2 an

d a temperature increase from 500 K to 1000 K. The path followed by the gas during compression is given by:
PV1.55 = constant

and the molar heat capacity of the gas is given by:

CP/R = 3.30 + 0.63x10-3 T (T in K)

Determine the final pressure and the heat transferred during the process.

Engineering
1 answer:
Mashutka [201]3 years ago
6 0

Answer:

attached below

Explanation:

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At a 4 percent annual growth rate in GDP per capita, it will take
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Answer:

At a 4 percent annual growth rate in GDP per capita, it will take 18 years for GDP per capita to double.

Explanation:

  • GDP stands for the gross domestic products. It is the basis to monitor the value of good and service in the market.
  • According to rule of 70:

Number of years to double = \frac{70}{annual growth rate}

                                             = \frac{70}{4}

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In this way in total of 18 years the GDP will be double at the constant annual growth rate of 4%.

8 0
2 years ago
Air is used as the working fluid in a simple ideal Brayton cycle that has a pressure ratio of 12, a compressor inlet temperature
7nadin3 [17]

Answer:

A) m' = 351.49 kg/s

B) m'= 1036.91 kg/s

Explanation:

We are given;

Pressure Ratio;r_p = 12

Inlet temperature of compressor;T1 = 300 K

Inlet temperature of turbine;T3 = 1000 K

cp = 1.005 kJ/kg·K

k = 1.4

Net power output; W' = 70 MW = 70000 KW

A) Now, the formula for the mass flow rate using the total power output of the compressor and turbine is given as;

m' = W'/[cp(T3(1 - r_p^(-(k - 1)/k)) - T1(r_p^((k - 1)/k))

At, 100% efficiency, plugging in the relevant values, we have;

m' = 70000/(1.005(1000(1 - 12^(-(1.4 - 1)/1.4)) - 300(12^((1.4 - 1)/1.4)))

m' = 70000/199.1508

m' = 351.49 kg/s

B) At 85% efficiency, the formula will now be;

m' = W'/[cp(ηT3(1 - r_p^(-(k - 1)/k)) - (T1/η) (r_p^((k - 1)/k))

Where η is efficiency = 0.85

Thus;

m' = 70000/(1.005(0.85*1000(1 - 12^(-(1.4 - 1)/1.4)) - (300/0.85)(12^((1.4 - 1)/1.4)))

m' = 70000/(1.005*(432.09129 - 364.9189)

m'= 1036.91 kg/s

4 0
3 years ago
At the inlet to the combustor of a supersonic combustion ramjet (or scramjet), the flow Mach number is supersonic. For a fuel-ai
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Answer:

The inlet match number is 3.42.

Explanation:

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Explain why different types of equipment are required for proper conditioning of air
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