DGCA Gas Turbine 6. The Exhaust System

 

Results

Q1. The velocity of the gases in the exhaust unit is held to:

Correct answer is – Mach 0.5 to minimize turbulence

Q2. The exhaust cone:

Correct answer is – prevents the hot gases flowing across the rear turbine face

Q3. The propelling nozzle is designed to:

Correct answer is – increase the velocity and decrease the pressure of the gas stream

Q4. A nozzle is said to be “choked” when:

Correct answer is – the gas flow through it reaches its sonic value

Q5. A choked nozzle:

Correct answer is – implies that no further increase in velocity can be obtained without the increase of heat

Q6. The exhaust gases pass to atmosphere via the propelling nozzle which:

Correct answer is – is a convergent duct, thus it increases the gas velocity

Q7. The jet pipe is insulated from the airframe by:

Correct answer is – a combination of cooling air and insulating material

Q8. The noise from a high ratio bypass engine:

Correct answer is – is predominantly from the fan and the turbine

Q9. The shape of the volume within the jet pipe casing immediately to the rear of the turbine:

Correct answer is – is divergent to reduce the velocity of the gases leaving the turbine

Q10. The turbine rear support struts:

Correct answer is – straighten out any residual whirl in the gas stream

Q11. An exhaust nozzle is said to be choked when the velocity at the throat is:

Correct answer is – at Mach 1

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