Unit 1 Flashcards

(20 cards)

1
Q

Angle of Attack is the angle between?

A

The chord line and relative wind

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2
Q

The angle of attack at which the airplane stalls

A

Is always the same and depends on the airfoil design

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3
Q

Induced drag is the result of

A

Generation of lift

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4
Q

Parasite drag is affected as follows by airspeed

A

As airspeed increases, parasite drag increases

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5
Q

To clear obstacles close to the departure end of the runway climb at

A

Vx

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6
Q

Adverse yaw during turn is caused by

A

Increased drag on the high wing

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7
Q

During a turn a steeper bank angle will result in

A

Increased rate of turn

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8
Q

The purpose of the elevator trim is to

A

Relieve the control pressures the pilot must hold

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9
Q

The function of the flaps is to

A

Allow flight at slower airspeed

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10
Q

If the ball in the turn and bank indicator is displaced to the right during a right turn

A

Increase right rudder input

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11
Q

During engine failure in flight, the best glide airspeed is the airspeed that results in

A

The longest glide distance

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12
Q

An airplane with CG close to its aft limit

A

Is less stable

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13
Q

To gain the most altitude in a specified time you must climb at

A

Vy

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14
Q

Ground effect when flying close to the ground is caused by

A

Change of the effective relative wind which results in less induced drag and increased lift

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15
Q

While taxiing you observe the wind is blowing from your front left. The controls must be held as follows

A

Yoke to the left, right ailerons down left up ( turn into the wind)

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16
Q

For the airplane to maintain constant speed climb

A

There must be excess power available than what is required for cruise flight

17
Q

The force that causes an airplane to turn is

A

The horizontal component of lift resulting from banking

18
Q

The direction of relative wind is

A

Opposite to the flight path

19
Q

Takeoff and landing is accomplished into wind to

A

Allow us to develop the requires lift at slow ground speed

20
Q

Wing washout refers to the

A

Decreasing angle of incidence from root to wingtip