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
lateral axis
axis from wing tip to wing tip
26
vertical axis
axis vertically through the aircraft center of gravity
27
roll
movement around the longitudinal axis (wing tips moving up or down)
28
pitching
movement around the lateral axis (nose or tail moving up or down)
29
yawing
movement around the vertical axis
30
roll is controlled by...
ailerons
31
pitch is controlled by..
elevators
32
yaw is controlled by...
rudder
33
What temperature of air creates more lift?
cooler air (it is more dense than warmer air)
34
primary control system
systems needed to control the airplane during flight (ailerons, elevator, rudder)
35
secondary control system
improve airplane performance (wing flaps, trim control systems)
36
What type of movement does the joystick control?
roll and pitch movements
37
What type of movement do the rudder pedals control?
yaw of the airplane
38
How does an aileron work to roll the aircraft?
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
angle of attack
angle between horizontal chord line and air foil
40
adverse yaw
when the nose of the aircraft yaws in the direction of the raised wing due to increased drag