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M15c1
15問 • 2ヶ月前
  • مقطع من الاغاني عراقيه قصيره
  • 通報

    問題一覧

  • 1

    Newton third law of motion

    For every action there is an equal and opposite reaction.

  • 2

    The working cycle of the heat engine as

    constant-pressure cycle.

  • 3

    Gas inside the combustion section of gas turbine engine

    reduce from front to rear.

  • 4

    Pressure in combustion chamber

    virtually constant

  • 5

    The rocket

    is a non-air breathing engine means it does not use atmospheric air to support combustion

  • 6

    Pulse Jet

    it has additional spring loaded valves in the air intake

  • 7

    The turbofan mixture of a

    turbojet and a turboprop, literally handles a hot air mass and a cold air mass.

  • 8

    always maintain high pressure compressor speed constant.

    Governor

  • 9

    A high bypass engine is more efficient because it is similar to the

    propeller by accelerating large mass of air at a low rate of acceleration.

  • 10

    Easier starting

    the small HP compressor only needs to be rotated by the starter

  • 11

    is gas coupling with compressor NOT mechanically connected.

    Free turbine

  • 12

    drives the output shaft which drives propeller in turbo-prop engine and rotor in turbo-shaft engines.

    Free turbine

  • 13

    By pass ratio 5:1

    indicates that bypass flow is five times the hot stream

  • 14

    1st digit represent the

    bypass air.

  • 15

    2nd digit represent to

    engine core air.

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    問題一覧

  • 1

    Newton third law of motion

    For every action there is an equal and opposite reaction.

  • 2

    The working cycle of the heat engine as

    constant-pressure cycle.

  • 3

    Gas inside the combustion section of gas turbine engine

    reduce from front to rear.

  • 4

    Pressure in combustion chamber

    virtually constant

  • 5

    The rocket

    is a non-air breathing engine means it does not use atmospheric air to support combustion

  • 6

    Pulse Jet

    it has additional spring loaded valves in the air intake

  • 7

    The turbofan mixture of a

    turbojet and a turboprop, literally handles a hot air mass and a cold air mass.

  • 8

    always maintain high pressure compressor speed constant.

    Governor

  • 9

    A high bypass engine is more efficient because it is similar to the

    propeller by accelerating large mass of air at a low rate of acceleration.

  • 10

    Easier starting

    the small HP compressor only needs to be rotated by the starter

  • 11

    is gas coupling with compressor NOT mechanically connected.

    Free turbine

  • 12

    drives the output shaft which drives propeller in turbo-prop engine and rotor in turbo-shaft engines.

    Free turbine

  • 13

    By pass ratio 5:1

    indicates that bypass flow is five times the hot stream

  • 14

    1st digit represent the

    bypass air.

  • 15

    2nd digit represent to

    engine core air.