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ASTB Week 3 > Aviation Information > Flashcards

Aviation Information Flashcards

1
Q

Types of Aviation

A

Civil and military

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2
Q

Fixed Wing

A

Fighter jets, bombers, airliners, and corporate jets

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3
Q

Rotary Wing

A

Helicopters, gyrocopters, and tilt-rotor flying machines

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4
Q

Airfoil

A

A wing or helicopter blade that generates more lift than drag as air flows over its upper and lower surfaces. A propeller is also an airfoil. Airfoils are carefully designed and can be made of non-metallic materials such as composites.

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5
Q

Angle of Attack

A

The angle between the chord line of an airfoil and its direction of motion relative to the air (i.e. the relative wind). AOA is an aerodynamic angle.

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6
Q

Angle of Incidence

A

In the context of fixed-wing airplanes, the angle of incidence is the inclination of the wing or tail surface attached to the fuselage relative to an imaginary line that is parallel to the aircraft’s longitudinal axis.

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7
Q

Anhedral Angle

A

The downward angle of an airplane’s wings and tail plane from the horizontal is called the anhedral angle, or negative dihedral angle.

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8
Q

Attitude

A

An aircraft’s position relative to its three axes and a reference as such as the earth’s horizon.

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9
Q

Center of Gravity (CG)

A

An aircraft’s center of mass, the theoretical point through which the entire weight of the machine is assumed to be concentrated.

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10
Q

Chord

A

The distance between the leading and trailing edges along the chord line is an airfoil’s chord. In the case of a tapered airfoil, as viewed from above, the chord at its tip will be different than at its root. Average chord describes the average distance.

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11
Q

Chord Line

A

An imaginary straight line from the airfoil’s leading (front) edge to its trailing (aft) edge.

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12
Q

Constant Speed Propeller

A

A controllable-pitch propeller whose angle is automatically changed in flight by a governor in order to maintain a constant number of revolutions per minute (rpm) despite changing aerodynamic loads.

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13
Q

Controllability

A

A measure of an aircraft’s response relative to flight control inputs from the pilot via a control in the cockpit.

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14
Q

Controllable Pitch Propeller

A

A propeller that can be varied in terms of its blade angle by the pilot via a control in the cockpit.

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15
Q

Coordinated Flight

A

When the pilot applies fight and power control inputs to prevent slipping or skidding during any aircraft maneuver, the flight is said to be coordinated.

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16
Q

Critical Angle of Attack

A

The angle of attack at which an airfoil stalls (loses lift) regardless of the aircraft’s airspeed, attitude, or weight.

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17
Q

Dihedral Angle

A

The upward angle of an airplane’s wings and tail plane from the horizontal.

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18
Q

Dihedral Effect

A

The amount of roll movement produced per degree pf sideslip is called dihedral effect, which is crucial in terms of an aircraft’s rolling stability about its longitudinal axis.

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19
Q

Directional Stability

A

An aircraft’s initial tendency about its yaw (vertical) axis. When an aircraft is disturbed yaw-wise from its equilibrium state, for example, and returns to the state (i.e. aligned with the relative wind) because of the aerodynamic effect of the vertical stabilizer, it is said to be directionally stable.

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20
Q

Downwash

A

Air that is deflected perpendicular to an airfoil’s motion.

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21
Q

Drag Coefficient

A

A dimensionless quantity that represents the drag generated by an airfoil of a particular design.

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22
Q

Drag Curve

A

A constructed image of the amount of aircraft drag at different airspeeds.

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23
Q

Dynamic Stability

A

Describes the tendency of an aircraft after it has been disturbed from straight-and-level flight to restore the aircraft to its original condition of flying straight and level by developing corrective forces and moments.

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24
Q

Equilibirum

A

In the context of aviation, equilibrium is an aircraft’s state when all opposing forces acting on it are balanced, resulting in unaccelerated flight at a constant altitude.

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25
Q

Feathering Propeller

A

A controllable-pitch propeller that can be rotated sufficiently by the pilot (via a control lever in the cockpit connected to a governor in the propeller hub) so that the blade angle is parallel to the line of flight, thereby minimizing propeller drag.

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26
Q

Forward Slip

A

A pilot-controlled maneuver where the aircraft’s longitudinal axis is inclined to its flight path.

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27
Q

Glide Ratio

A

The ratio between altitude lost and distance traversed during non-powered flight (e.g. following an engine failure, in a sailplane).

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28
Q

Glidepath

A

An aircraft’s path’s across the ground while approaching to land.

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29
Q

Gross Weight

A

An aircraft’s total weight when it is fully loaded with aircrew, fuel, oil, passengers and/or cargo (if applicable), weapons, etc.

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30
Q

Gyroscopic Procession

A

The attribute of rotating bodies to manifest movement ninety degrees in the direction of rotation from the point where a force is applied to the spinning body.

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31
Q

Heading

A

The direction in which the aircraft’s nose is pointed.

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32
Q

Inertia

A

A body’s opposition to change in motion.

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33
Q

Internal Combustion Engine

A

A mechanical device that produces power from expanding hot gases created by burning a fuel-air mixture within the device.

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34
Q

Lateral Stability (Rolling)

A

An aircraft’s initial tendency relative to its longitudinal axis after being disturbed, its designed quality to return to level flight following a disturbance such as a gust that causes one of the aircraft’s wings to drop.

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35
Q

Lift Coefficient

A

A dimensionless quantity that represents the lift generated by an airfoil of a particular design.

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36
Q

Lift/Drag Ratio

A

A number that represents an airfoil’s efficiency, the ratio of the lift coefficient to the drag coefficient for a specific angle of attack.

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37
Q

Lift-Off

A

The act of rising from the earth as a result of airfoils lifting the aircraft above the ground.

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38
Q

Load Factor

A

The ratio of load supported by an aircraft’s lift-generating airfoils (wings, main rotor blades) to the aircraft’s actual weight, including the mass of its contents. Load factor is also known as G-Loading (“G” means gravity).

39
Q

Longitudinal Stablility

A

An aircraft’s initial tendency relative to its lateral axis after being disturbed, its designed quality to return to its trimmed angle of attack after being disrupted due to a wind gust or other factor.

40
Q

Maneuverability

A

An aircraft’s ability to change directions in three axes along its flight path and withstand the associated aerodynamic forces.

41
Q

Mean Camber Line

A

An imaginary line between the leading and the trailing edges and halfway between the airfoil’s upper (curved) and lower (flat) surfaces.

42
Q

Minimum Drag Speed (L/DMAX)

A

The point on the total drag curve where total drag is minimized and lift is maximized (i.e., where the lift-to-drag ratio is greatest).

43
Q

Nacelle

A

An enclosure made of metal or another durable material that covers an aircraft engine.

44
Q

Non-Symmetrical Airfoil (Cambered)

A

When one surface of an airfoil has a specific curvature that the opposite side does not, the airfoil is described as non-symmetrical, or cambered. The advantage of a non-symmetrical, for example, is that it produces lift at an AOA of zero degrees (as long as airflow is moving past the blade). Moreover, the lift-to-drag ratio and stall characteristics of a cambered airfoil are better than those of a symmetrical airfoil. Its disadvantages are center of the pressure movement chord-wise by as much as one-fifth the chord line distance, which causes undesirable airfoil torsion, and greater production costs.

45
Q

Normal Category

A

An airplane intended for non-acrobatic operation that seats a maximum of nine passengers and had a certificated takeoff weight of 12,500 pounds or less.

46
Q

Payload

A

In the context of aviation, the weight of an aircraft’s occupants, cargo, and baggage.

47
Q

P-Factor (Precession Factor)

A

A propeller-driven aircraft’s tendency to yaw to the left when the propeller rotates clockwise (as seen by the pilot) because the descending propeller blade on the right produces more thrust than the ascending blade on the left. If the propeller rotated counter-clockwise, the yaw tendency would be to the right.

48
Q

Piston Engine

A

Also known as the reciprocating engine, it is a heat engine that uses one or more pistons to convert pressure by creating expanded, hot gases resulting from a combusted fuel-air mixture, or steam pressure, into a rotating motion.

49
Q

Pitch

A

An airplane’s rotation above its lateral axis, or the angle of a propeller blade as measured from the vertical plane of rotation.

50
Q

Power Lever

A

The cockpit lever connected to a turbine engine’s fuel control unit, which changes the amount of fuel entering the combustion chambers.

51
Q

Powerplant

A

An engine and its accessories (e.g., starter-generator, tachometer drive) and the attached propeller (usually via a gearbox).

52
Q

Propeller Blade Angle

A

The angle between the chord of an airplane propeller blade and the propeller’s plane of rotation.

53
Q

Propeller Lever

A

The cockpit control that controls propeller speed and angle.

54
Q

Propeller Slipstream

A

Air accelerated behind a spinning propeller.

55
Q

Propeller

A

A relatively long and narrow blade-like device that produces thrust when it rotates rapidly. In aviation, the term typically includes not only the propeller blades but also the hub and other components that make up the propeller system.

56
Q

Rate of Turn

A

The rate if a turn expressed in degrees per second.

57
Q

Reciprocating Engine

A

An engine that converts heat energy created by combusted fuel mixed with air into reciprocating piston movement, which in turn is converted into a rotary motion via a crankshaft.

58
Q

Reduction Gear

A

A gear or set of gears that turns a propeller at a speed slower than that of the engine.

59
Q

Relative Wind

A

The direction of airflow relative to an airfoil, a stream of air parallel and opposite to an aircraft’s flight path.

60
Q

Ruddervator

A

Two control surfaces on an aircraft’s tail that form a V. When moved together via the control wheel or joystick in the cockpit, the surfaces act as elevators. When the pilot presses his or her foot against one rudder pedal or the other, the ruddervator acts like a conventional plane’s rudder.

61
Q

Sideslip

A

A flight maneuver controlled by the pilot that involves the airplane’s longitudinal axis remaining parallel to the original flight path, but the aircraft no longer flies forward, as in normal flight. Instead, the horizontal lift component causes the plane to move laterally toward the low wing.

62
Q

Skid

A

A flight condition during a turn where the airplane’s tail follows a path outside of the path of the aircraft’s nose.

63
Q

Slip

A

A maneuver used by pilots to increase an aircraft’s rate of descent or reduce its airspeed, and to compensate for a crosswind during landing. An unintentional slip occurs when a pilot does not fly the aircraft in a coordinated manner.

64
Q

Stability

A

An aircraft’s inherent tendency to return to its original flight path after a force such as a wind gust disrupts its equilibrium. Aeronautical engineers design most aircraft to be aerodynamically stable.

65
Q

Stall

A

A rapid decrease in lift caused by an excessive angle of attack and airflow separating from an airfoil’s upper surface. An aircraft can stall at any pitch attitude or airspeed.

66
Q

Standard-Rate Turn

A

A rate of turn of three degrees per second.

67
Q

Subsonic

A

Speed below the speed of sound, which varies with altitude.

68
Q

Supersonic

A

Speed in excess of the speed of sound, which varies with altitude.

69
Q

Swept Wing

A

A wing platform involving the tips being further back than the wing root.

70
Q

Symmetrical Airfoil

A

When an airfoil has identical upper and lower surfaces, it is symmetrical and produces no lift at an AOA of zero degrees. The wings of very high performance aircraft tend to be symmetrical.

71
Q

Taxiway Lights

A

Blue lights installed at taxiway edges.

72
Q

Taxiway Turn Off Lights

A

Green lights installed level with the taxiway.

73
Q

Throttle

A

A mechanical device that meters the amount of fuel-air mixture fed to the engine.

74
Q

Thrust Line

A

An imaginary line through the center of an airplane’s propeller hub and perpendicular to the propeller’s plane of rotation, or through the center of each jet engine.

75
Q

Total Aerodynamic Force (TAF)

A

Two components comprise the total aerodynamic force: lift and drag. The amount of lift and drag produced by an airfoil are the primarily determined by its shape and area.

76
Q

Torque

A

A propeller driven airplane’s tendency to roll in the opposite direction of the propeller’s rotation. Some multi-engine airplanes have propellers that rotate in opposite directions to eliminate the torque effect.

77
Q

Trailing Edge

A

The aft part of an airfoil where air that was separated as it hit the wing’s front edge was forced over the upper and lower surfaces comes together.

78
Q

Transonic

A

At the speed of sound, which varies with altitude.

79
Q

Trim Tab

A

A small, hinged control surface on a larger control surface (e.g., aileron, rudder, elevator) that can be adjusted in flight to a position that balances the aerodynamic forces. In still air, a trimmed aircraft in flight requires no control inputs from the pilot to remain straight and level.

80
Q

T-Tail

A

The description for an airplane’s tail involving the horizontal stabilizer mounted on the top of the vertical stabilizer.

81
Q

Turbulence

A

The unsteady flow of a fluid or gas (e.g., water or air).

82
Q

Utility Category

A

An airplane intended for limited acrobatic operation that seats a maximum of 9 passengers and has a certificated takeoff weight of 12.5 thousand pounds or less.

83
Q

Vector

A

A force applied in a certain direction. Depicted visually, a vector shows the force’s magnitude and direction.

84
Q

Velocity

A

The rate of movement (e.g., miles per hour, knots) in a certain direction.

85
Q

Vertical Stability

A

An aircraft’s designed, inherent behavior relative to its vertical axis, its tendency to return to its former heading after being disturbed by a wind gust or other disruptive force. Also called yawning or directional stability.

86
Q

V-Tail

A

A design involving two slanted tail surfaces that aerodynamically behave similar to a conventional elevator and rudder, i.e., as horizontal and vertical stabilizer.

87
Q

Wing

A

An airfoil attached to a fuselage that creates a lifting force when the aircraft has reached a certain speed.

88
Q

Wing Area

A

A wing’s total surface, including its control surfaces, and winglets, if so equipped.

89
Q

Wing In Ground Effect (WIG)

A

When an aircraft flies at a very low altitude, one roughly equal to its wingspan, it experiences WIG. The effect increases as the airplane descends closer to the surface (runway, land, water) and supports the aircraft on a cushion of air best at an altitude of one half the wing span.

90
Q

Winglet

A

A surface installed on a wingtip that is angled to the wing and improves its efficiency by smoothing the airflow across the upper wing near the tip and reducing induced drag. Winglets improve an aircraft’s lift-to-drag ratio.

91
Q

Wing Span

A

The maximum distance between wingtips.

92
Q

Wingtip Vortices

A

A spinning mass of air generated at a wing’s tip created by outward-flowing high pressure air from underneath the wing meeting inward-flowing low air pressure on the wing’s upper surface. The intensity of a wing vortex - also referred to as wake turbulence - is dependent on an airplane’s weight, speed, and configuration.

93
Q

Wing Twist

A

A wing design feature that improves the effectiveness of aileron control at high angles of attack during an approach to a stall.

ASTB Week 3 (3 decks)

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