ASA Ch 1 Flashcards

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1
Q

Chord line

A

A straight line from the leading edge to the trailing edge of an airfoil

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2
Q

Airfoil

A

A structure or body which produces a useful reaction to air movement

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3
Q

Relative wind

A

The wind felt by an airfoil, created by the movement of air past the airfoil, by the motion of the airfoil through the air, or by a combination of the two

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4
Q

Angle of attack

A

The angle between the chord line of the airfoil and the relative wind

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5
Q

Angle of incidence

A

The angle at which a wing is attached to the fuselage

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6
Q

Lateral axis

A

A line from wingtip to wingtip

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7
Q

Pitch

A

Rotation around the lateral axis

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8
Q

Longitudinal control

A

Control of pitch, aka longitudinal stability

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9
Q

Longitudinal axis

A

A line from nose to tail

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10
Q

Roll

A

Rotation around the longitudinal axis

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11
Q

Lateral control

A

Control of roll, aka lateral stability

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12
Q

Vertical axis

A

A line extending vertically through the intersection of the lateral and longitudinal axes

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13
Q

Yaw

A

Rotation around the vertical axis

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14
Q

Directional control

A

Control of yaw, aka directional stability

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15
Q

Center of gravity

A

The point at which an airplane would balance if it were suspended at that point, and the intersection of the lateral, longitudinal, and vertical axes

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16
Q

Weight

A

The downward-acting force of gravity

17
Q

Lift

A

The upward-acting force which allows the airplane to become airborne

18
Q

Drag

A

The rearward-acting force which resists the plane’s forward movement

19
Q

Thrust

A

The forward-acting force created by the propeller

20
Q

Bernoulli’s Principle

A

As the velocity of a fluid increases, its pressure decreases

21
Q

Parasite drag

A

That portion of drag produced by the resistance of the air against any part of the plane that does not produce lift

22
Q

Induced drag

A

Drag created as a by-product of lift

23
Q

Stability

A

The inherent ability of an airplane to return (or not return) to its original flight condition after being disturbed by an outside force such as rough air

24
Q

Positive static stability

A

The initial tendency of an aircraft to return or not return to its original position

25
Q

Positive dynamic stability

A

The tendency of an oscillating airplane to return to its original position relative to time

26
Q

Horizontal lift component

A

The portion of lift created by the wings which is diverted into a sideways force when the airplane is banked into a turn

27
Q

Vertical lift component

A

The portion of lift created by the wings which is countering the effects of gravity on the plane

28
Q

Load

A

The force that must be supported by an airplane structure in flight

29
Q

Centrifugal force

A

Force which pushes toward the outside of a curve when an airplane is flying a curved path (turns, climbs, descents)

30
Q

Load factor

A

Load imposed on the wings in flight

31
Q

Stall

A

Loss of lift sufficient to make flight unsustainable

32
Q

Critical angle of attack

A

The angle of attack at which a stall occurs

33
Q

Ground effect

A

When flying one wingspan or less above the surface, the airflow around the wing and wing tips is modified and the resulting pattern reduces downwash and induced drag. Can result in airplane becoming airborne before recommended takeoff speed or floating during approach to land

34
Q

Wake turbulence

A

Areas behind a moving aircraft in which the air is moving in unpredictable or dangerous ways

35
Q

Wingtip vortices

A

A byproduct of lift in which air twirls in a vortex behind the tip of each wing