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JNTU B.Tech II THERMODYNAMICS FOR AEROSPACE ENGINEERING Previous Question Paper (February - 2024 - R22)

B.Tech | II | II-I | R22 | February - 2024

Answer PaperPaper Code: 183CHMaximum Marks: 60Time: 3 Hours

Note: This question paper contains two parts A and B. Part-A is a compulsory question. Part-B consists of ten questions (numbered from 2 to 11) carrying 10 marks each. From each unit, there are two questions, and the student should answer one of them. Hence, the student should answer five questions from Part-B.

Part A

110 marks
a

Define Zeroth law of Thermodynamics.

1 marks

Answer

The Zeroth Law of Thermodynamics states that if two systems are each in thermal equilibrium with a third system, they are in thermal equilibrium with each other.

b

Differentiate between extensive and intensive property.

1 marks

Answer

An intensive property is independent of the mass of the system (e.g., pressure, temperature), whereas an extensive property depends on the total mass or size of the system (e.g., total volume, total energy).

c

State Kelvin Planck’s Statement of second Law.

1 marks

Answer

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d

What is the corollary of Carnot’s Theorem?

1 marks

Answer

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e

Define latent heat of sublimation and dryness fraction.

1 marks

Answer

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f

What is a pure substance?

1 marks

Answer

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g

What do you mean by regeneration?

1 marks

Answer

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h

State the four processes of Diesel cycle.

1 marks

Answer

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i

What do you understand by dry and wet compression?

1 marks

Answer

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j

What are the most widely used refrigerants?

1 marks

Answer

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Part B

2

A steam turbine drives a ship’s propeller through an 8: 1 reduction gear. The average resisting torque imposed by the water on the propeller is 750 × 103 Nm and the shaft power delivered by the turbine to the reduction gear is 15 MW. The turbine speed is 1450 rpm. Determine (a) the torque developed by the turbine, (b) the power delivered to the propeller shaft, and (c) the net rate of working of the reduction gear.

10 marks

Answer

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OR
310 marks
a

Derive an expression of Steady flow energy equation for a single stream entering and a single stream leaving a control volume.

5 marks

Answer

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b

If a gas of volume 6000 cm3 and at pressure of 100 kPa is compressed quasi-statically according to

pV2 = constant
until the volume becomes 2000 cm3, determine the final pressure and the work transfer.

5 marks

Answer

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4

If 20 kJ are added to a Carnot cycle at a temperature of 100°C and 14.6 kJ are rejected at 0°C, determine the location of absolute zero on the Celsius scale.

10 marks

Answer

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OR
510 marks
a

Discuss in detail with the help of mathematical expression about the maximum work in a reversible process.

5 marks

Answer

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b

Prove that the COP of a reversible refrigerator operating between two given temperatures is the maximum.

5 marks

Answer

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610 marks
a

Draw the phase equilibrium diagram for a pure substance on p-T coordinates. Why does the fusion line for water have negative slope?

5 marks

Answer

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b

A rigid vessel of volume 0.86 m3 contains 1 kg of steam at a pressure of 2 bar. Evaluate the specific volume, temperature, dryness fraction, internal energy, enthalpy, and entropy of steam.

5 marks

Answer

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OR
7

A rigid vessel contains 1 kg of a mixture of saturated water and saturated steam at a pressure of 0.15 MPa. When the mixture is heated, the state passes through the critical point. Determine: a) The volume of the vessel b) The mass of liquid and of vapour in the vessel initially.

10 marks

Answer

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8

Obtain an expression for the specific work done by an engine working on the Otto cycle in terms of the maximum and minimum Temperatures of the cycle, the compression ratio rk, and constants of the working fluid. Hence show the compression ratio for maximum specific work output.

10 marks

Answer

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OR
9

An air standard limited pressure cycle has a compression ratio of 15 and compression begins at 0.1 MPa, 40°C. The maximum pressure is limited to 6 MPa and the heat added is 1.675 MJ/kg. Compute (a) the heat supplied at constant volume per kg of air, (b) the heat supplied at constant pressure per kg of air, (c) the work done per kg of air, (d) the cycle efficiency, (e) the temperature at the end of the constant volume heating process, (f) the cut-off ratio, and (g) the m.e.p. of the cycle.

10 marks

Answer

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10

A Refrigerant-12 vapour compression cycle has a refrigeration load of 3 tonnes. The evaporator and condenser temperatures are – 20°C and 40°C respectively. Find (a) The refrigerant flow rate in kg/s (b) The volume flow rate handled by the compressor in m3/s (c) The work input to the compressor in kW (d) The heat rejected in the condenser in kW (e) The isentropic discharge temperature. If there is 5° C of superheating of vapour before it enters the compressor, and 5°C sub cooling of liquid before it flows through the expansion valve, determine the above quantities.

10 marks

Answer

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OR
11

A vapour compression refrigeration system uses R-12 and operates between pressure limits of 0.745 and 0.15 MPa. The vapour entering the compressor has a temperature of – 10°C and the liquid leaving the condenser is at 28°C. A refrigerating load of 2 kW is required. Determine the COP and the swept volume of the compressor if it has a volumetric efficiency of 76% and runs at 600 rpm.

10 marks

Answer

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About this paper

This page contains the question paper of THERMODYNAMICS FOR AEROSPACE ENGINEERING from JNTU for B.Tech AE II II-I, February - 2024, R22.

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