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lord [1]
3 years ago
12

Steam enters a turbine operating at steady state at 600°F and 200 lbf/in^2 with a velocity of 80 ft/s and leaves as saturated va

por at 5 lbf/in^2 with a velocity of 300 ft/s. The power developed by the turbine is 200 horsepower. Heat transfer from the turbine to the surroundings occurs at a rate of 50,000 Btu/h.
a. Neglecting potential energy effects, determine the mass flow rate of steam, in lb/s.
Engineering
1 answer:
MissTica3 years ago
8 0

Answer:

49.05 lb / s

Explanation:

Given:

Inlet 1

P_1 = 200 psia

T_1 = 600 F

V_1 = 80 ft / s

Exit 2

P_2 = 5 psia

saturated vapor

V_2 = 300 ft / s

Power W = 200-hp = 509000 Btu/h = 8483.333 Btu / s

Heat Loss Q = 50,000 Btu / h = 833.3333 Btu / s

Solution:

From Table A-6E for steam inlet conditions:

h_1 = 1322.3 Btu / lbm

From Table A-5E for steam inlet conditions:

h_2 = 1130.7 Btu / lbm

Energy Balance:

Q - W = m_flow *( (h_2 - h_1) + (V_2^2 - V_1^2) / 2*25037)

m_flow = ( Q - W ) / ((h_2 - h_1) + (V_2^2 - V_1^2) / 2*25037)

m_flow = ( - 833.333 - 8483.33) / ((1130.7-1322.3) + (300^2-80^2)/50074)

m_flow = -9316.66663 / -189.9305

m_flow = 49.05 lb/s

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An air-standard Diesel cycle engine operates as follows: The temperatures at the beginning and end of the compression stroke are
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This question is incomplete, the complete question is;

An air-standard Diesel cycle engine operates as follows: The temperatures at the beginning and end of the compression stroke are 30 °C and 700 °C, respectively. The net work per cycle is 590.1 kJ/kg, and the heat transfer input per cycle is 925 kJ/kg. Determine the a) compression ratio, b) maximum temperature of the cycle, and c) the cutoff ratio, v3/v2.

Use the cold air standard assumptions.

Answer:

a) The compression ratio is 18.48

b) The maximum temperature of the cycle is 1893.4 K

c) The cutoff ratio, v₃/v₂ is 1.946

Explanation:

Given the data in the question;

Temperature at the start of a compression T₁ = 30°C = (30 + 273) = 303 K

Temperature at the end of a compression T₂ = 700°C = (700 + 273) = 973 K

Net work per cycle W_{net = 590.1 kJ/kg

Heat transfer input per cycle Qs = 925 kJ/kg

a) compression ratio;

As illustrated in the diagram below, 1 - 2 is adiabatic compression;

so,

Tγ^{Y-1 = constant { For Air, γ = 1.4 }

hence;

⇒ V₁ / V₂ = ( T₂ / T₁ )^{\frac{1}{Y-1}

so we substitute

⇒ V₁ / V₂ = (  973 K / 303 K  )^{\frac{1}{1.4-1}

= (  3.21122  )^{\frac{1}{0.4}

= 18.4788 ≈ 18.48

Therefore, The compression ratio is 18.48

b) maximum temperature of the cycle

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we substitute

925 = 1.005( T₃ - 700 )

( T₃ - 700 ) = 925 / 1.005

( T₃ - 700 ) = 920.398

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T₃ = ( 1620.398 + 273 ) K

T₃ = 1893.396 K ≈ 1893.4 K

Therefore, The maximum temperature of the cycle is 1893.4 K

c)  the cutoff ratio, v₃/v₂;

Since pressure is constant, V ∝ T

So,

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we substitute

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cutoff ratio S = 1.9459 ≈ 1.946

Therefore, the cutoff ratio, v₃/v₂ is 1.946

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