Theory of Flights Flashcards

(73 cards)

1
Q

Described bird flight as the combined effect of the action of the individual feathers as they twist and turn during flight and the complex flapping of the wings.

A

1680 of Giovanni Borelli’s De Motu Animalum

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2
Q

Ancestors of modern aviation and airplane

A

kites

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3
Q

Year kites are flown and where

A

400 BC in China

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4
Q

When and Who put on a pair of wings and leapt

A

1020 AD Oliver of Malmesbury

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5
Q

Worked with Air, Pressure, and steam to create sources of power

A

Ancient Greek Engineer Heron Alexandrinus

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6
Q

Experiment which used hets of steam to create a rotary motion

A

aeolipile or Hero’s engine

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7
Q

who designed the first successful flying craft

A

Joseph and Jacques Montgolfier

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8
Q

The first aviators

A

duck, rooster, and sheep

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9
Q

First who discovered how wings work

A

Sir George Cayley

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10
Q

Sentence that set in motion the future study of aerodynamics

A

“The whole problem is confined within these limits, namely to make a surface support a given weight by the application of power to the resistance of air”

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11
Q

Time and Date of of the first successful airplane

A

10:35 am on December 17, 1903

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12
Q

Name of the first successful airplane

A

Flyer

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13
Q

Who made the world’s first successful airplane

A

Orville and Wilbur Wright

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14
Q

Describe the first airplane

A

Has own engine that weighed 200 pounds, 4 cylinders, make 12 horsepower. Has no seat and had to lay in the bottom wing.

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15
Q

three sectors of aviation community

A

commercial aviation, general aviation, military aviation

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16
Q

what is commercial aviation

A

airplane for hire, can fly domestically or internationally

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17
Q

what is general aviation

A

non-commercial business flights, aerial work, instructional and pleasure flying and other flying

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18
Q

what is military aviation

A

search and rescue operation, disaster operation, crash and retrieval operation, dog military operation.

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19
Q

two categories of aircraft

A

lighter-than-air aircraft and heavier-than-air aircraft

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20
Q

powered aircraft with a wing and tail

A

airplane

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21
Q

aircraft having no engine which is capable of free flight only while it is descending through the air

A

glider / sailplanes / seaplane

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22
Q

A machine that can drive support in the atmosphere from the reactions of the air than the reactions of the air against the earth’s surface. A weight carry structure, supported by its own buoyancy or by the dynamic action of the air against its surfaces, intended for navigation in the air.

A

aircraft

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23
Q

widely known as conventional airplane having fuselage, wings and empennage

A

airplane

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24
Q

It’s a non-power-driven aircraft, deriving its lift in flight chiefly from aerodynamic reactions on surface which remain fixed and conditions of flight.

A

gliders

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25
a type of aerostat or lighter-than-air aircraft that can navigate through the air under its own power.
airships
26
It is also defined as the type of aircraft of the same design including all modifications there to except those modifications which result in a change in handling or flight characteristics.
heavier-than-air aircraft
27
have the fewest operating limitations because their design requirements demand more strength than those of normal or utility airplanes "an intentional maneuver involving an abrupt change in an aircraft's attitude, an abnormal attitude, or abnormal acceleration, not necessary for normal flight."
aerobatic airplane
28
aircraft designed to fly short, frequent routes from a small airport to a larger hub airport. Small airports have shorter runways which may limit the largest commuter aircraft to regional jets or turboprop-powered planes with nineteen (19) passengers or less.
commuter airplane
29
usually refers to airliners and other large airplanes that exceed certain weight limits of 8,619 kilograms or more than the passenger-carrying capacity more than 19 seats.
transport airplane
30
is for special purpose airplane such as agricultural spray airplane or slurry bombers to fight forest fires.
restricted airplane
31
an aircraft that has not yet been fully proven in flight. Often, this implies that new aerospace technologies are being tested on the aircraft, though the label is broader.
experimental aircraft
32
major components of an aircraft
powerplant, wing, empennage, fuselage, landing gears
33
central body of an airplane and is designed to accommodate the crew, passengers, and cargo. It also provides the structural connection for the wings and tail assembly. Older types of aircraft design utilized an open truss structure constructed of wood, steel, or aluminum tubing.
fuselage
34
airfoils attached to each side of the fuselage and are the main lifting surfaces that support the airplane in flight . may be attached at the top, middle, or lower portion of the fuselage. These designs are referred to as high-, mid-, and low-wing, respectively . The number of wings can also vary.
wing
35
principal structural parts of the wings
spars, ribs, stringers
36
determine the shape and thickness of the wing (airfoil)
wing ribs
37
are either an integral part of the wing’s structure or consist of flexible containers mounted inside of the wing.
fuel tanks
38
includes the entire tail group and consists of fixed surfaces, such as the vertical stabilizer and the horizontal stabilizer. The movable surfaces include the rudder, the elevator, and one or more trim tabs.
empennage
39
principal support of the airplane when parked, taxiing, taking off, or landing.
landing gear
40
usually includes both the engine and the propeller. The primary function of the engine is to provide the power to turn the propeller.
powerplant
41
mounted on the front of the engine, translates the rotating force of the engine into thrust, a forward acting force that helps move the airplane through the air. rotating airfoil that produces thrust through aerodynamic action
propeller
42
any surface, such as wing, which provides aerodynamic force when it interacts with a moving stream of air.
airfoil
43
this part of the airfoil meets the airflow first.
leading edge
44
this is the portion of the airfoil where the airflow over the upper surface rejoins the lower surface airflow.
trailing edge
45
is an imaginary straight line drawn through an airfoil from the leading edge to the trailing edge.
chord line
46
the characteristic curve of its upper and lower surfaces.
camber
47
this is the direction of the airflow with respect to the wing.
relative wind
48
this is the angle between the chordline of the airfoil and the direction of the relative wind.
angle of attack
49
distinguished by having identical upper and lower surfaces. The mean camber line and chord line are the same on a symmetrical airfoil, and it produces no lift at zero AOA. Most light helicopters incorporate symmetrical airfoils in the main rotor blades.
symmetrical airfoil
50
has different upper and lower surfaces, with a greater curvature of the airfoil above the chord line than below. The mean camber line and chord line are different. The nonsymmetrical airfoil design can produce useful lift at zero AOA. A nonsymmetrical design has advantages and disadvantages.
nonsymmetrical airfoil (cambered)
51
refers to the shape of the airplane’s wing when viewed from above and below.
planform
52
affects the difference in the velocity of the airflow between the upper and lower surfaces of the wing. If the upper camber increases and the lower camber remains the same, the velocity differential increases.
camber
53
is the relationship between the length and width of the wing. It is one of the primary factors in determining lift/drag characteristics.
aspect ratio
54
total surface area of the wings. Most wing don’t produce a great amount of lift per square foot, so wing area must be sufficient to support the weight of the airplane.
wing area
55
burning created gas causing a craft to rise.
Montgolfier's gas
56
known as father of aviation
George Cayley
57
constructed the first aircraft that was heavier than air
George Cayley
58
issues licenses as regards to the repair, alteration, inspection, and maintenance of military airplanes.
Civil Aviation Authority of the Philippines
59
easily recognized by its large overhead propeller called rotor
rotary wing aircraft
60
have powered rotor both vertical and horizontal motion through the air
helicopters
61
type of rotorcraft whose main rotors are not connected to the engine except for the initial spin up. Aerodynamic forces causes the main rotor for spin during normal light
gyroplanes
62
airplanes with a single set of wings
monoplane
63
airplanes with two sets of wings
biplanes
64
most type of landing gear
wheels
65
landing gears for water
floats
66
landing gears for snow
skis
67
It also generates electrical power, provides a vacuum source for some flight instruments, and in most single-engine airplanes, provides a source of heat for the pilot and passengers.
powerplant
68
direction of the relative wind and flight path
relative wind is upward and back while flight path is parallel to and opposite.
69
when the angle of attack increases, what increases?
lift
70
how does the lift act towards the relative wind
parallel
71
formula of the aspect ratio
span / average chord
72
the higher the aspect ratio, the higher is what?
lifting efficiency
73
explain the bernoulli's principle
the higher the velocity, the lower the pressure and the lower the velocity, the higher the pressure