
Airplane Wings and Their Functions
Presentation
•
Science
•
9th - 12th Grade
•
Hard
Joseph Anderson
FREE Resource
40 Slides • 14 Questions
1
Parts of an Aircraft
© 2011 Project Lead The Way, Inc.
Flight and Space
2
What is an Airplane?
• Aircraft
– More general term
– Refers to any heavier-than-air object that is
• Supported by its own buoyancy
• Supported by the action of air on its structures
• Airplane
– Heavier-than-air craft propelled by an engine
– Uses aerodynamic surfaces (wings) to
generate lift
3
What is an Airplane?
Every airplane is an aircraft, but not every
aircraft is an airplane.
– Space shuttle
– Gliders
– Helicopters
4
Why So Many Types?
Every modern aircraft is built for a specific
purpose.
– Different altitudes
– Different speeds
– Different weight-carrying capacities
– Different performance
5
Why So Many Types?
• Jet fighters
– Relatively lightweight
– Highly maneuverable and very fast
– Carry small amount of weight, including fuel
– Must refuel on long flights
• Passenger airplanes
– Larger, carry more weight, fly longer distances
– Less maneuverable and slower
6
Why So Many Types?
• Wing types
7
Why So Many Types?
Speed
– The speed of sound is dependent on altitude
and atmospheric conditions
– Mach is the term used to specify how many
times the speed of sound an aircraft is
traveling
– Subsonic:
Less than Mach 1
– Transonic: Mach .8 to Mach 1.2
– Supersonic: All speeds above Mach 1
– Hypersonic: All speeds greater than Mach 5
8
Parts of an Airplane
• Five basic structural components
– Fuselage
– Wings
– Empennage (tail structures)
– Propulsion system
– Undercarriage
9
Aircraft Components
Five typical components
Empennage
Fuselage
Wing
Landing
Gear
Power Plant
10
Fuselage
• Main body structure
– All other components are attached to it
• Contains
– Cockpit or flight deck
– Passenger compartment
– Cargo compartment
• Produces a little lift, but can also produce
a lot of drag
11
Rigid framework made up of members, such as beams, struts, and bars to resist deformation by applied loads. It was commonly used in early aircraft days for airplanes such as Wright Flyer and Douglas DC-3.
Open Truss
Types Of Fuselage
Pros :
relatively simple and easy to construct.
Spreads force evenly between members
Cons:
Produce more drag
Weight Distribution and Balance
Can't sustain high speeds (large surface area)
Noisy
High Vibration
12
makes use of a space frame formed from a spirally crossing basket-weave of load-bearing members. Pioneered by British aeronautical engineer Barnes Wallis in the 1930s.
Geodesic
Types Of Fuselage
Pros :
light and strong
Large Internal Volume
Durable
Cons:
Expensive cost and maintenance
Assembly was time consuming
isn't suitable for higher-flying, pressurized aircraft.
13
(single shell) fuselage relies largely on the strength of the skin or covering to carry the primary loads. uses formers, frame assemblies, and bulkheads to give shape to the fuselage.
Monocoque
Types Of Fuselage
Pros :
Strong structure
Lightweight
Internal Volume
Cons:
Damage to the skin can compromise the entire structure
14
Consists of frame assemblies, bulkheads, and formers as used in the monocoque design but, additionally, the skin is reinforced by longitudinal members called longerons.
Semi-monocoque
Pro:
Overcome the strength/weight problem of monocoque
cost-effective and easier to produce
Cons:
Weight
Complex constructs
Types Of Fuselage
15
Multiple Choice
An aircraft's main body structure housing the flight crew, passengers, and cargo
Wing
Fuselage
Empennage
Horizontal stabilizer
Vertical stabilizer
16
17
Wings
• Most important lift-producing part of the
aircraft
• Also carries the fuel
• Designed so that the outer tips of the
wings are higher than where the wings are
attached to the fuselage
– Called the dihedral
– Helps keep the airplane from rolling
unexpectedly
18
19
20
21
Multiple Choice
The main lifting surface of an airplane
Wing
Fuselage
Empennage
Horizontal stabilizer
Vertical stabilizer
22
Multiple Choice
An aircraft's tail group. Includes the rudder, elevators, horizontal and vertical stabilizers
Wing
Fuselage
Empennage
Horizontal stabilizer
Vertical stabilizer
23
Multiple Choice
The fixed part of a horizontal airfoil that controls the pitch of an aircraft
Wing
Fuselage
Empennage
Horizontal stabilizer
Vertical stabilizer
24
Multiple Choice
The fixed part of a vertical airfoil that controls the yaw of an aircraft
Wing
Fuselage
Empennage
Horizontal stabilizer
Vertical stabilizer
25
Multiple Choice
Supports the aircraft when it is not in the air, allowing it to take off, land, and taxi on the ground without damage
Trailing edge
Leading edge
Airfoil
Landing gear
Propeller
26
Multiple Choice
A device for propelling an aircraft that has blades on an engine-driven shaft and that, when rotated, produces thrust
Trailing edge
Leading edge
Airfoil
Landing gear
Propeller
27
Wings
28
Type of aircraft with a single pair of wings. Its main feature uses the airflow between adjacent wings reduces efficiency.
Monoplane
an aircraft with two wings, one above the other, it main feature was maneuverability but couldn't offset the speed advantage of the lighter monoplane
Biplane
An aircraft with three vertically stacked wing planes, its main feature was generating greater lift power due to large size and extra wings
Triplane
Wing Number
29
Wing Designs
• Straight Wing
– Found mostly on small,
low-speed airplanes
– Good lift at low speeds
– Not suited to high speeds
– Creates a lot of drag because
the wing is perpendicular to
the airflow
– Provides good, stable flight
– Cheap and can be made
lighter
30
Wing Designs
• Sweepback
– Used on most high-speed
airplanes
– Less drag, but more unstable at
low speeds
– Amount of sweep depends on
the purpose of the airplane
• Commercial airliner has moderate
sweep
• High speed airplanes (e.g.,
fighters) have moderate sweep
• No forward sweep wings are in
mass production
31
Wing Designs
• Delta Wings
– Looks like a large triangle
from above
– Can reach high speeds
– Landing speeds are very
fast
– Wing shape found on the
supersonic transport
Concord
32
Wing Designs
• Swing Wing
– This design combines the
high lift characteristics of a
straight wing with the ability
of the sweepback wing to
move at high speeds
– During landing and takeoff,
wing swings into an almost
straight position
– During cruise, wing swings
into a sweepback
– Hinges that enable wings to
swing are very heavy
33
Wing Components
• Trailing edge
equipped with flaps
– Move backward and
downward
– Increase the area of
the wing and the
camber of the airfoil
– Different from the
ailerons, also located
on the trailing edge of
the wing
34
Wing Components
• Slats
– Located on the
leading edge
– Slide forward and
increase the area of
the wing and the camber of the airfoil
• Flaps and slats
– Used during takeoff and landing
– Increase lift at slower speeds.
35
Wing Components
36
Wing Components
• Spoilers
– Located on the top of the wings
– Opposite effect from flaps and slats
– Reduce lift by disrupting the airflow over the
top of the wing
– Deployed after the
airplane has landed
and lift is no longer
needed
– Increase drag
37
Empennage
• Also known as the tail
assembly
• Provides stability and
control
• Two main parts
– Vertical stabilizer (fin) to
which the rudder is
attached
– Horizontal stabilizer to
which the elevators are
attached
38
Undercarriage
• Also known as the landing gear, which is
made up of
– Struts
– Wheels
– Brakes
• Can be fixed or
retractable
39
Propulsion System
• Provides thrust for the airplane
• Many different types of engines
– Piston engines and propellers
– Turboprop
– Turbojet
– Turbofan
– Scram jet
• These will be discussed in a later activity.
40
Controls
• Instruments and Controls
– Supply information
• Altitude
• Direction
– Provide control
• Steering in the air
and on the ground
• Engine power
• Braking
41
Controls
42
Controls
• Roll is controlled by the ailerons
– Used to raise and lower the wings
Turning the control wheel left
causes the left aileron to raise
and lowers the right aileron.
The plane rolls left.
Turning the control wheel right
causes the right aileron to raise
and lowers the left aileron.
The plane rolls right.
43
Controls
• Pitch is controlled by the elevators on the
tail of the plane.
• They are controlled by the control wheel
(i.e., stick).
If the wheel or stick is pushed
forward, the elevators go down,
causing the nose to point down
and the plane to lose altitude.
If the wheel or stick is pulled back,
the elevators go up, causing the
nose to point up and the plane to
climb.
44
Controls
• Yaw is controlled by the rudder.
• The right foot pedal turns the rudder to the
right.
• This action causes the tail to yaw to the
left and the nose to yaw to the right.
To smoothly bank a plane
or to turn it left or right, the
pilot uses the ailerons and
the rudder together.
45
46
Controls
• On the ground, the plane’s direction is
controlled by steering the nose wheel.
Pilots use their feet on the rudder
pedals to control the ground movement
• The rudder pedals are
also used to apply the
brakes.
47
Image Resources
Microsoft, Inc. (2008). Clip art. Retrieved June 24, 2009, from
http://office.microsoft.com/en-us/clipart/default.aspx
National Aeronautics and Space Administration (NASA). (n.d.). Virtual
skies: Aeronautics tutorial. Retrieved June 24, 2009, from
http://virtualskies.arc.nasa.gov/aeronautics/tutorial/intro.html
48
Multiple Choice
Which airplane motion is controlled by the elevators?
Roll
Pitch
Yaw
49
Multiple Choice
Which airplane motion is controlled by the rudder?
Roll
Pitch
Yaw
50
Multiple Choice
Which airplane motion is controlled by the rudder?
Roll
Pitch
Yaw
51
Multiple Choice
Which airplane motion is controlled by the ailerons?
Roll
Pitch
Yaw
52
Multiple Choice
This surface controls pitch about the lateral axis of the aircraft
Ailerons
Elevators
Rudder
Flaps
53
Multiple Choice
This surface controls yaw about the vertical axis of the aircraft
Ailerons
Elevators
Rudder
Flaps
54
Multiple Choice
This surface controls roll about the longitudinal axis of the aircraft
Ailerons
Elevators
Rudder
Flaps
Parts of an Aircraft
© 2011 Project Lead The Way, Inc.
Flight and Space
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