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TECH GENERAL — CH.20

The Air InletAircraft & Engines — DGCA CPL practice questions

Question 1 of 4

A subsonic engine intake is shaped as a:

A.Convergent duct
B.Divergent duct
C.Convergent-divergent duct
D.Straight pipe

All 4 questions — The Air Inlet

Aircraft & Engines · DGCA CPL. The correct option is marked on each.

  1. Q1. A subsonic engine intake is shaped as a:

    • A.Convergent duct
    • B.Divergent duct
    • C.Convergent-divergent duct
    • D.Straight pipe

    Why: The divergent intake slows ram air and raises its pressure before the compressor — ram pressure recovery.

  2. Q2. Supersonic intakes use movable ramps or spikes to:

    • A.Increase the airflow velocity
    • B.Control shockwave position and slow the air to subsonic speed
    • C.Filter out foreign objects
    • D.Generate extra thrust

    Why: Compressors cannot accept supersonic flow; the intake geometry manages shockwaves to decelerate the air efficiently.

  3. Q3. Engine intake anti-icing typically uses:

    • A.Electrical heater mats only
    • B.Hot bleed air from the compressor
    • C.De-icing boots
    • D.Glycol spray

    Why: Hot compressor bleed air heats the intake lip to stop ice forming and being ingested into the compressor.

  4. Q4. FOD refers to:

    • A.Fan Overspeed Detection
    • B.Foreign Object Damage from debris entering the intake
    • C.Fuel On Demand
    • D.Flight Operations Directive

    Why: Stones, birds and other debris entering the intake can severely damage compressor blades — Foreign Object Damage.