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m.8.4
27問 • 1年前
  • Slem Abdo
    • 通報

    問題一覧

  • 1

    Rate of climb is dependent upon

    excess power.

  • 2

    In straight and level flight

    lift = weight, and thrust = drag.

  • 3

    The glide ratio is the same as the

    lift/drag ratio

  • 4

    The best gliding angle is achieved by using the angle of attack that gives

    the best L/D ratio

  • 5

    Compared to straight and level flight, when an aeroplane is turning

    stall speed increases and load factor increases.

  • 6

    During a turn, for any given speed

    the radius of turn will depend upon the angle of bank

  • 7

    A minimum radius turn is easier achieved

    at low altitude

  • 8

    An increase in altitude will cause the rate of turn

    to decrease

  • 9

    To achieve a maximum rate turn, it can be shown that

    Wing loading must be as low as possible.

  • 10

    Flaps at landing position

    decrease landing speed.

  • 11

    The load factor of a given aircraft in a given condition of flight is defined as

    the lift divided by the weight.

  • 12

    During a turn

    insufficient rudder causes slip

  • 13

    Fowler flap

    increases the area of the wing.

  • 14

    A winglet

    reduces drag and increases thrust.

  • 15

    Winglets

    reduce tip vortices, increasing the effective aspect ratio

  • 16

    Ground effect results

    in increased lift and reduced drag.

  • 17

    In the case of an aircraft making a turn, the force causing centripetal acceleration

    is the horizontal component of the lift acting on the aircraft.

  • 18

    A standard rate turn is defined as a 3° per second turn, which completes a 360° turn in 2 minutes.

    This is known as a 2-minute turn or rate one (180°/min).

  • 19

    The power provided by jet and piston engines alike decrease with altitude,

    due mainly to decreasing air density

  • 20

    When an aeroplane is in an unpowered descent, a component of the weight

    acts forwards along the flight path, and provides the ‘thrust’ to drive the aeroplane forwards against the drag.

  • 21

    In any manoeuvre, the stalling speed is

    proportional to the square root of the load factor

  • 22

    When a turn is executed without any skid or slip, it

    is called a coordinated turn

  • 23

    Directional stability is stability about

    the normal axis

  • 24

    Passive stability

    the inherent stability incorporated into an aeroplane by the aerodynamic features and the configuration of the aeroplane

  • 25

    The normal axis of an aircraft passes

    through the center of gravity

  • 26

    If the aeroplane is loaded with the centre of gravity too far aft,

    the aeroplane may assume a nose up rather than a nose down attitude.

  • 27

    Porpoising

    If the aeroplane is loaded with the centre of gravity too far aft,

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    問題一覧

  • 1

    Rate of climb is dependent upon

    excess power.

  • 2

    In straight and level flight

    lift = weight, and thrust = drag.

  • 3

    The glide ratio is the same as the

    lift/drag ratio

  • 4

    The best gliding angle is achieved by using the angle of attack that gives

    the best L/D ratio

  • 5

    Compared to straight and level flight, when an aeroplane is turning

    stall speed increases and load factor increases.

  • 6

    During a turn, for any given speed

    the radius of turn will depend upon the angle of bank

  • 7

    A minimum radius turn is easier achieved

    at low altitude

  • 8

    An increase in altitude will cause the rate of turn

    to decrease

  • 9

    To achieve a maximum rate turn, it can be shown that

    Wing loading must be as low as possible.

  • 10

    Flaps at landing position

    decrease landing speed.

  • 11

    The load factor of a given aircraft in a given condition of flight is defined as

    the lift divided by the weight.

  • 12

    During a turn

    insufficient rudder causes slip

  • 13

    Fowler flap

    increases the area of the wing.

  • 14

    A winglet

    reduces drag and increases thrust.

  • 15

    Winglets

    reduce tip vortices, increasing the effective aspect ratio

  • 16

    Ground effect results

    in increased lift and reduced drag.

  • 17

    In the case of an aircraft making a turn, the force causing centripetal acceleration

    is the horizontal component of the lift acting on the aircraft.

  • 18

    A standard rate turn is defined as a 3° per second turn, which completes a 360° turn in 2 minutes.

    This is known as a 2-minute turn or rate one (180°/min).

  • 19

    The power provided by jet and piston engines alike decrease with altitude,

    due mainly to decreasing air density

  • 20

    When an aeroplane is in an unpowered descent, a component of the weight

    acts forwards along the flight path, and provides the ‘thrust’ to drive the aeroplane forwards against the drag.

  • 21

    In any manoeuvre, the stalling speed is

    proportional to the square root of the load factor

  • 22

    When a turn is executed without any skid or slip, it

    is called a coordinated turn

  • 23

    Directional stability is stability about

    the normal axis

  • 24

    Passive stability

    the inherent stability incorporated into an aeroplane by the aerodynamic features and the configuration of the aeroplane

  • 25

    The normal axis of an aircraft passes

    through the center of gravity

  • 26

    If the aeroplane is loaded with the centre of gravity too far aft,

    the aeroplane may assume a nose up rather than a nose down attitude.

  • 27

    Porpoising

    If the aeroplane is loaded with the centre of gravity too far aft,