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TaAP - Brayton and Engines

Total questions: 11

Worksheet time: 4mins

Name
Class
Date
1.

The efficiency of the Brayton cycle is always _ the efficiency of the Carnot cycle.

a)

equal to

b)

greater than

c)

double

d)

less than

2.

Which process is represented by 1-2 in the Brayton cycle diagram?

a)

isobaric compression

b)

isothermal compression

c)

isentropic compression

d)

isochoric compression

3.

Which processes shown in the Brayton cycle diagram are isobaric?

a)

2-3 and 4-1

b)

1-2 and 2-3

c)

3-4 and 4-1

d)

1-2 and 3-4

4.

A gas turbine engine has a pressure ratio of 26. Assuming the engine cycle can be represented by the air-standard Brayton cycle, what will be the cycle efficiency?

a)

26%

b)

60.6%

c)

0.6%

d)

74%

5.

The Brayton cycle diagram shown represents which gas turbine hardware?

a)

1-2: combustion, 2-3: compressor, 3-4: exhaust, 4-1: turbine

b)

1-2: turbine, 2-3: exhaust, 3-4: compressor, 4-1: combustion

c)

1-2: exhaust, 2-3: compressor, 3-4: combustion, 4-1: turbine

d)

1-2: compressor, 2-3: combustion, 3-4: turbine, 4-1: exhaust

6.

Turboprops are most efficient in:

a)

High speed, high altitude operations.

b)

Low speed, low altitude operations.

7.

Which of the following is most efficient at high speeds?

a)

Turbo-prop

b)

Low by-pass turbofan

c)

High by-pass turbofan

d)

Pure turbojet

8.

For a thermodynamically ideal turbo-jet, the process that occurs through the outlet nozzle is:

a)

isentropic compression

b)

isothermal compression

c)

isentropic expansion

d)

isothermal expansion

9.

Which of the following features 'supersonic combustion'?

a)

High by-pass turbofans

b)

Scramjets

c)

Ramjets

d)

Pure turbojets

10.

For a thermodynamically ideal turbo-jet, the combustion process can be considered:

a)

adiabatic

b)

isentropic

c)

isothermal

d)

isobaric

11.

This diagram is representative of which type of engine?

a)

A ramjet

b)

A low by-pass turbofan

c)

A scramjet

d)

A pure turbojet