Brayton – Cycle Analysis, Performance and Comparison

Brayton – Cycle Analysis, Performance and Comparison

1st Grade

5 Qs

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Brayton – Cycle Analysis, Performance and Comparison

Brayton – Cycle Analysis, Performance and Comparison

Assessment

Quiz

Education

1st Grade

Medium

Created by

SIVASHANKAR M

Used 1+ times

FREE Resource

5 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the main principle behind the thermodynamics of the Brayton Cycle?

Entropy always increases

Conservation of mass

Conservation of energy

Second law of thermodynamics

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How is the efficiency of the Brayton Cycle calculated?

Efficiency = 1 - (1 / compression ratio)^((gamma-1)/gamma)

Efficiency = 1 - (compression ratio)^((gamma-1)/gamma)

Efficiency = 1 - (1 / compression ratio)^((gamma-1)*gamma)

Efficiency = 1 - (1 / compression ratio)^((gamma+1)/gamma)

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Name one performance parameter used to evaluate the Brayton Cycle.

Thermal efficiency

Inlet temperature

Pressure ratio

Specific work output

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What are the key differences between an ideal and an actual Brayton Cycle?

The key differences are: 1. Isentropic vs. irreversible compression and expansion processes. 2. No pressure losses vs. pressure drops in compressor and turbine. 3. Higher thermal efficiency in ideal cycle.

Lower thermal efficiency in ideal cycle

No heat addition vs. heat addition in combustion chamber

Adiabatic vs. isothermal compression and expansion processes

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Explain why the Brayton Cycle is commonly used in gas turbine engines.

The Brayton Cycle is commonly used in gas turbine engines because it is environmentally friendly.

The Brayton Cycle is commonly used in gas turbine engines due to its low efficiency and power output.

The Brayton Cycle is commonly used in gas turbine engines due to its high efficiency and power output.

The Brayton Cycle is commonly used in gas turbine engines because it is cheap to implement.