Exhaust Section, Reverse Thrust

Exhaust Section, Reverse Thrust

Professional Development

22 Qs

quiz-placeholder

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Exhaust Section, Reverse Thrust

Exhaust Section, Reverse Thrust

Assessment

Quiz

Professional Development

Professional Development

Medium

Created by

Theory Lecturer

Used 10+ times

FREE Resource

22 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What happens when exhaust velocity is greater than forward speed?

Thrust

Deceleration

Engine overheating

Stress cracking from rapid cooling

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What happens at the exhaust of a converging/diverging ducted exhaust?

Pressure decreases, velocity increases

Pressure increases, velocity increases

Pressure increases, velocity decreases

Pressure decreases, velocity decreases

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The velocity of the gases in the exhaust unit is held to:

Mach 0.5 to minimize turbulence

Mach 0.75 to optimize the pressure distribution

Mach 0.85 to maximize thrust

Mach 1 to maximize acceleration

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The exhaust cone:

straightens the gas flow before it goes into the turbine assembly

prevents the hot gases flowing across the rear turbine face

increases the velocity of the gases

decreases the pressure of the gas

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What exhaust system does a high-performance military jet use?

Convergent-divergent

Convergent

Divergent

Divergent-convergent

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How do designers reduce noise produced by turbine engines?

Reduce exhaust gas velocity

Increase Exhaust gas temp

Use a convergent divergent duct

Increase exhaust velocity

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Use of reverse thrust below the recommended speed may cause:

over stressing of the gear oleos.

ingestion of the exhaust gases and foreign objects.

more fuel to be provided to the burners.

the TGT limit to be exceeded, in which case the reverse thrust lever will return to the forward thrust position.

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