Flight Theory and Movements Flashcards

1
Q

Newton’s First Law of Motion

A

a body at rest tends to stay at rest and a body in motion tends to stay in motion (inertia)

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2
Q

Newton’s Second Law

A

F=ma; acceleration is directly proportional to the force applied and inversely proportional to the mass of the object

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3
Q

Newton’s Third Law

A

for every action there is an equal and opposite reaction

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4
Q

Four Forces which act on an aircraft in flight

A

lift, gravity (weight), thrust, drag

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5
Q

lift

A

pushes the aircraft up

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6
Q

weight

A

pulls the aircraft down

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7
Q

thrust

A

pushes the aircraft forward

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8
Q

drag

A

slows the aircraft or pushes it back

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9
Q

flight envelope

A

the different combinations of the four factors that allow the aircraft to be flown safely; ex flying out of the envelope is slang for unsafe conditions

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10
Q

Use Newton’s laws to describe why planes can fly

A

the wing splits the air (action) and lift is the reaction; there is a net change in the air after it passes over the wing to a reaction force acts of the wing giving it lift; lift is produced by diverting air downward

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11
Q

upwash

A

oncoming air stream the is deflected upward and over the wing

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12
Q

trailing edge

A

where the airflow that cam over the top of the wing rejoins the lower surface first

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13
Q

leading edge

A

the part of the airfoil which meed the airflow first

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14
Q

downwash

A

downward air stream deflection as it passes over the wing and past the trailing edge

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15
Q

stall

A

separation of airflow from the wings upper surface creating a rapid decrease in lift; happens from the trailing edge coming forward; happens slowly;

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16
Q

how to recover from a stall

A

the pilot has to restore smooth airflow by decreasing the angle of attack below the stalling angle

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17
Q

how to tell if there is a stall

A

mushiness in controls of slight buffeting of the aircraft

18
Q

basic weight

A

weight of the aircraft plus weapons, unusable fuel, oil, equipment etc that will stay on the plane during flight

19
Q

operating weight

A

sum of basic weight and items such as crew, baggage, emergency equipment, all other non expendable items not in basic weight

20
Q

gross weight

A

total weight of the aircraft including contents and mounted items, anytime

21
Q

landing gross weight

A

weight of the aircraft, plus contents and external items when it lands

22
Q

zero fuel weight (ZFW)

A

weight of aircraft without any usable fuel

23
Q

induced drag

A

drag that is a result of lift

24
Q

longitudinal axis

A

axis through the fuselage from nose to tail

25
Q

lateral axis

A

axis from wing tip to wing tip

26
Q

vertical axis

A

axis vertically through the aircraft center of gravity

27
Q

roll

A

movement around the longitudinal axis (wing tips moving up or down)

28
Q

pitching

A

movement around the lateral axis (nose or tail moving up or down)

29
Q

yawing

A

movement around the vertical axis

30
Q

roll is controlled by…

A

ailerons

31
Q

pitch is controlled by..

A

elevators

32
Q

yaw is controlled by…

A

rudder

33
Q

What temperature of air creates more lift?

A

cooler air (it is more dense than warmer air)

34
Q

primary control system

A

systems needed to control the airplane during flight (ailerons, elevator, rudder)

35
Q

secondary control system

A

improve airplane performance (wing flaps, trim control systems)

36
Q

What type of movement does the joystick control?

A

roll and pitch movements

37
Q

What type of movement do the rudder pedals control?

A

yaw of the airplane

38
Q

How does an aileron work to roll the aircraft?

A

One aileron will go up and the other will go down, the one that goes up decreases the lift on that side making that wing drop; the one that goes down increases the lift and makes that wing go up

39
Q

angle of attack

A

angle between horizontal chord line and air foil

40
Q

adverse yaw

A

when the nose of the aircraft yaws in the direction of the raised wing due to increased drag