Wing Design
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Transcript of Wing Design
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WING DESIGN
By Kudzai Mutasa, Victor Oluyede, Patrick Palmer and Andre Nicholson
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WING DESIGN 2
How do wings work?
• Wing shape enables air to travel at different speeds
• Different speeds create a pressure differential
• Differential pushes wing up and we have flight!
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WING DESIGN 3
Aspects of Wing Design
Plan form Number of wings Wing Vertical Position Aspect Ratio Airfoils and flattening Flaps and Other High Lift Devices
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WING DESIGN 4
Planform
This is the wing shape as seen from above
Primary purpose is to increase maximum speed of aircraft
Greater sweep leads to air reaching wings at a slower time
Hence aircraft can reach greater top speeds
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WING DESIGN 5
Planform
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Aspect Ratio•Its is the ratio of the wing span(S) to the wing mean aerodynamic chord(C)•A high aspect ratio indicates long, narrow wings, whereas a low aspect ratio indicates short, stubby wings.[1]
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Aspect Ratio
Air escapes at wing tips creating ”vortices.”
Lower pressure at wing tips reduces overall lift
Greater aspect ratio= greater high pressure to low pressure ratio
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WING DESIGN 8
Number of wings
3 types : Monoplane (One wing),Biplane (Two wings) and Tri-plane (Three wings)
Disadvantages of having more than one wing -higher weight, lower lift and limited pilot visibility
A single wing usually has a longer wing span than two wings with the same total area.
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WING DESIGN 9
Wing vertical position
4 types: High wing Low wing Mid wing and Parasol wing Wing vertical location enables the
design of other aircraft components including aircraft tail and landing gear designs and the centre of gravity.
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WING DESIGN 10
Wing vertical position
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WING DESIGN 11
Airfoils
Airfoil-the shape of a wing as seen in cross-section.
Aerofoil designs differ depending on their purpose
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WING DESIGN 12
Airfoils(continued)
An airfoil-shaped body moved through a fluid produces two aerodynamic forces when thrust is applied
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WING DESIGN 13
Airfoils(continued)
Lift is produced primarily through deflection
Cambered aerofoils can produce lift at a zero angle of attack based on Bernoulli’s principle
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WING DESIGN 14
Flattening
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Flattening
Also known as arc The more you arc you apply the worse
performance you get. The advantages are indirect: more arc
stiffens and smoothens the wing by causing the tips to fly apart, stretching the fabric.
With a more stable wing designers can increase the aspect ratio
Positives outweigh negatives
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WING DESIGN 16
Flattening- examples
Example of high arc next to normal arc glider
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WING DESIGN 17
High Lift Devices
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The Equation Of Lift
L = Lift, which must equal the airplane's weight in Newton's
d = density of the air. This will change due to altitude.
v = velocity in metres per second s = the wing area in square metres CL = Coefficient of lift , determined by the type of
airfoil and angle of attack. Increasing the area (S) and lift coefficient (CL) allows
a similar amount of lift to be generated at a lower airspeed (V).
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Flaps•Most common high-lift devices used on aircraft. •Attached to the trailing edge of the wing and increase both lift and induced drag for any given AOA.• Allow for a compromise between high cruising speed and low landing speed•May be extended when needed, and retracted into the wing’ s structure when not needed.
•The Fowler flap is the type of airplane flap found on most jet aircraft. Fowler flaps are embedded in the wing, allowing for a minimal amount of drag while the aircraft is in cruise flight, a critical feature for a high-speed jet.
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Leading edge slats•Slats are aerodynamic surfaces on the leading edge of the wings of fixed-wing aircraftWhen deployed, they allow the wing to operate at a higher AOA. A higher coefficient of lift is produced as a result of the AOA and speed, • By deploying slats an aircraft can fly at slower speeds, or take off and land in shorter distances.• They are usually used while landing or performing manoeuvres which take the aircraft close to the stall, but are usually retracted in normal flight to minimize drag.
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WING DESIGN 21
Conclusion
The primary function of a wing is to generate lift
Wing design focuses on generating maximum lift with minimum drag
Engineers have come up with various ways of modifying wing capabilities
Aircraft wings can be fine-tuned for different purposes
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WING DESIGN 22
References
http://www.stockcarscience.com/blog/index.php/talladega_f09
http://rewston-stock.deviantart.com/art/Wing-stock-14-55600948
http://publicola.com/2009/09/22/it-was-the-strangest-thing-id-ever-heard/
http://weblab.open.ac.uk/firstflight/forces/
http://www.wainfan.com/wingdes.pdf http://upload.wikimedia.org/wikipedia/co
mmons/thumb/c/c9/Wing_profile_nomenclature.svg/500px-Wing_profile_nomenclature.svg.png
http://upload.wikimedia.org/wikipedia/commons/thumb/e/ee/Aeroforces.svg/220px-Aeroforces.svg.png