AMT 114 THEORY OF FLIGHT WITH WEIGHT AND BALANCE Flashcards

1
Q

Leonardo da Vinci made the first real studies of
flight in the 1480’s. He had over 100 drawings that
illustrated his theories on flight.

A

Ornithopter - 15th Century CE

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2
Q

The brothers, Joseph Michel and Jacques Etienne Montgolfier, were inventors of the first hot air balloon. They used the smoke from a fire to blow hot air into a silk bag. The silk bag was attached to a basket. The hot air then rose and allowed the balloon to be lighter-than-air.

A

Montgolfier Balloon - 1783

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3
Q

The discovery of the ____ that could fly in the air by the Chinese started humans’ thinking about flying.

A

Kite - 5th Century BC

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4
Q

he worked to discover a way that man could fly. He designed many different versions of gliders that used the movements of the body to control. A young boy, whose name is not known, was the first to fly one of his gliders.

A

Sir George Cayley - 1792

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5
Q

For many centuries, humans have tried to fly just
like the birds. Wings made of feathers or light
weight wood have been attached to arms to test
their ability to fly. The results were often disastrous
as the muscles of the human arms are not like a birds and can not move with the strength of a bird.

A

Tower Jumping - 852 CE

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6
Q

German engineer, _________, studied aerodynamics and worked to design a glider that would fly. He was the first person to design a glider
that could fly a person and was able to fly long distances.

A

Otto Lilienthal -1881-1896

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7
Q

any vehicle that is able to fly by gaining support
from the air.

A

The Aircraft

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8
Q

was never actually created. It was a design that Leonardo da Vinci
created to show how man could fly. The modern day helicopter is based on this concept.

A

Ornithopter flying machine

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9
Q

were used by the Chinese in religious
ceremonies. They built many colorful _____ for fun,
also. More sophisticated _____ were used to test
weather conditions. _____ have been important to the invention of flight as they were the forerunner
to balloons and gliders.

A

Kites

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10
Q

First, they read about all the early developments of flight. They decided to make “a small contribution” to the study of flight control
by twisting their wings in flight. Then they began to test their ideas with a kite. They learned about how the wind would help with the flight and how it could affect the surfaces once up in the air.

A

Wright Brothers - 1903

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11
Q

where they worked for two more years perfecting their design. Finally, on October 5, 1905, Wilbur piloted the Flyer III for 39 minutes and about 24 miles of circles around Huffman Prairie. He flew the first practical
airplane until it ran out of gas.

A

Wright Brothers

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12
Q

Parts of an Aircraft:

A

Powerplant, Wings, Empennage, Landing gear, Fuselage

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13
Q

He was fascinated by the idea of flight. Based on his
studies of birds and how they fly, he wrote a book on aerodynamics that was published in 1889 and this
text was used by the Wright Brothers as the basis
for their designs.

A

Otto Lilienthal -1881-1896

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14
Q

Classes of Airplane:

A

-Single Engine - Land
-Single Engine - Sea
-Multi Engine - Land
-Multi Engine - Sea

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15
Q

4 Categories of Aircraft:

A
  • Airplane
    -Rotorcraft
    -Glider
    -Lighter than Air
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16
Q

In 1783, the first passengers in the colorful balloon were a sheep, rooster and duck. It climbed to a height of about 6,000 feet and traveled more than 1 mile. After this first success, the brothers began to send men up in balloons.

A

Montgolfier Balloon - 1783

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17
Q

They designed and used a wind tunnel to test the shapes of the wings and the tails of the gliders. In 1902, with a perfected glider shape, they turned their attention to how to create a propulsion system that would create the thrust needed to fly.

A

Wright Brothers - 1903

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18
Q

The first manned flight was on ________, the passengers were Jean- Francois Pilatre de Rozier and Francois Laurent.

A

November 21, 1783

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19
Q

The ____ lifted from level ground to the north of
Big Kill Devil Hill, North Carolina, at 10:35 a.m., on December 17, 1903.

A

Flyer

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20
Q

The first heavier-than-air flight traveled one hundred twenty feet in twelve seconds. The _____ brothers took turns flying that day with the fourth and last flight covering 850 feet in 59 seconds. But
the Flyer was unstable and very hard to control.

A

Wright Brothers

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21
Q

Over 50 years he made improvements to the gliders. He changed the shape of the wings so that the air would flow over the wings correctly. He designed a tail for the gliders to help with the stability. He tried a biplane design to add strength to the glider. He also recognized that there would be a need for power if the flight was to be in the air for a long time.

A

Sir George Cayley - 1792

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22
Q

The early engine that they designed generated almost 12 horsepower. That’s the same power as two hand-propelled lawn mower engines!

A

Wright Brothers

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23
Q

After more than 2500 flights, he was killed when he lost control because of a sudden strong wind and crashed into the ground.

A

Otto Lilienthal -1881-1896

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24
Q

were very deliberate in their quest for flight.

A

Wright Brothers - 1903

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25
Q

Categories of Airplane:

A
  • Normal - max of +3.8Gs and -1.52Gs
  • Utility - max of +4.4Gs and -1.75Gs
    -Acrobatic - max of 6Gs and -3Gs
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26
Q

Fuselage Construction

A

Truss type
- Heavy
- Very Sturdy
(Longerons, Struts, Bulkhead, Stringers)

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27
Q

Types of Airplane (It is the maker or manufacturer and the model of
the airplane):

A

Cessna 152
Boeing 787
Airbus A350

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28
Q

is the central body of an airplane and is designed to accommodate the crew, passengers, and cargo.

A

Fuselage

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29
Q

Monocoque Parts and classifications

A
  • Light
  • Not Very Durable
    Stressed skin, Formers, Bulkhead
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30
Q

Semi Monocoque parts:

A

Stringers, Bulkhead, Skin, Formers

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31
Q

Wing support:

A

-Cantilever wing
-Semi Cantilever

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32
Q

Are airfoils attached to each side of the fuselage and are the main lifting surfaces that support the airplane in flight.

A

Wings

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32
Q
  • Lighter than Truss
    Type
A

Semi-Monocoque

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33
Q

Wing Location:

A

-Low wing
-Mid Wing
-High Wing

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34
Q

Parts of Wings:

A

Wing flap, Spar, Alteron, Fuel tank, Skin, Ribs, Stringers, Wing tip

35
Q

S t u r d i e r t h a n
Monocoque

A

Semi-Monocoque (Fuselage)

36
Q

Number of Wings

A

-Monoplane
-Biplane

37
Q

Wing Aspect Ratio

A

-Low aspect Ratio, Moderate aspect Ratio, High Aspect Ratio

38
Q

Landing Gear Positions:

A

Conventional, Tricycle Type

39
Q

Primary function is to provide the power to turn the propeller

A

Powerplant

40
Q

Empennage Parts:

A

Horizontal stabilizer, Vertical stabilizer, Rudder, Trim Tabs, Elevator

41
Q

Wing Sweep:

A

Straight, Sweptback

42
Q

Classification of Landing Gear

A

Rectractable landing gear, Fix gear

43
Q

is the upward force created by wings as the air
flows around them and it keeps the airplane in the air

A

Lift

44
Q

Wing Planform:

A

Constant, Tapered

45
Q

Types of Landing Gear:

A

Floats, Skis, Wheels

46
Q
  • is the forward force and created by the aircraft’s
    propellers or turbine engine.
A

Thrust

47
Q

it contains -stabilizers, elevators, rudder, trim tabs

A

The Empennage

48
Q

Usually includes both the engine and the propeller

A

Powerplant

49
Q

Four forces of Flight

A

Lift, Weight, Thrust, Drag

50
Q

is the force acting in the direction opposite of the thrust
which limits the performance of the airplane.

A

Drag

51
Q

Lift force =?

A

Weight Force

52
Q
  • is the downward force toward the center of the earth and is opposite of lift. It exists due to gravity
A

Weight

53
Q

When an aircraft is maintaining its heading, altitude,
and airspeed.

A

Straight-and-Level, Unaccelerated Flight

54
Q

is Perpendicular to the Relative Wind

A

Lift

55
Q

can be liquid, gas, or plasma

A

Fluids

56
Q

Thrust Force =?

A

Drag force

57
Q

Two Major Theories on Lift:

A
  1. Newton’s Third Law of Motion
  2. Bernoulli’s Principle
58
Q

The key to an aircraft’s ability to fly is “___”

A

Lift

59
Q

is a surface that generates an aerodynamic force as a fluid moves around it.

A

Airfoil

60
Q

“For every action, there is an equal and opposite reaction

A

Newton’s Third Law of Motion

61
Q

Top part of an airfoil

A

Upper Camber

62
Q

are any substance that deform under an applied stress

A

Fluids

63
Q

is produced due to the airfoil shape.

A

Lift

64
Q

Aft most point of an airfoil

A

Trailing Edge

65
Q

as the airplane flies through the air the path that the airplane travels along is know as its _____

A

Flight Path

66
Q
  • angle between the chord line and the relative wind
A

Angle of Attack

67
Q

Forward most point of an airfoil

A

Leading Edge

68
Q
  • Line from Leading Edge to Trailing Edge
A

Chord line

69
Q

airflow that flows around the airplane as it travel
through the air, and is in the opposite direction of the flight path

A

Relative Wind

70
Q

Bottom part of an airfoil

A

Lower Camber

71
Q

states that areas with highpressure moves to areas with low pressure. Since the wing is in between the low and high
pressures, it is therefore lifted up.

A

Pressure gradient force

72
Q

This states that,
“as the velocity of fluid (air)
increases, its internal pressure decreases”

A

Bernoulli’s Principle (The Venturi Effect)

73
Q

Due to the shape of the airfoil, the air travelling at the top of the airfoil will increase in speed which results in a lower pressure as compared to the pressure
below the airfoil. This imbalance is called _______

A

pressure gradient force.

74
Q

This change in pressure happens due to expansion and compression of fluids.

A

Bernoulli’s Principle (The Venturi Effect)

75
Q

As air flows around a wing, the air gets deflected downward which results it in lifting (opposite
reaction) the wing

A

Newton’s Third Law of Motion

76
Q

Engineer’s Formula
L= CL
(1/2)(ρ)(V2)(S)
L= Lift
CL=Coefficient of Lift
ρ = air density
V = velocity of the aircraft
S = Surface area of the Wing

A
77
Q

Is an event where the
wing stops generating
enough lift to keep the
aircraft flying.

A

Stall

78
Q

High angle of attack
Decreasing airspeed
Sluggish controls
Stall Horn
Buffeting or Vibration
Nose down
Negative VSI

A

Signs of Stall

79
Q

Heart of the aircraft

A

propeller

80
Q

Happens when the
critical angle of attack
is reached.

A

Stall

81
Q

2 types of airfoil:

A

Symmetrical, Asymmetrical

82
Q

L =?
CL=?
p=?
V=?
S=?

A

Lift, Coefficient of Lift, Air Density (rho), Velocity of the aircraft, Surface area of wind

83
Q

Lift Formula = ?

A

L = CL (1/2) (p)(V2)(S)

84
Q

What are the signs of stall:

A

High angle of attack
Decreasing airspeed
Sluggish controls
Stall Horn
Buffeting or Vibration
Nose down
Negative VSI

85
Q

Movement on the ground without any support

A

Taxi