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Tough question to answer as asked. In normal airfoils, the top of the airfoil is thicker and curved and it is this thicker, curved section that causes the air to speed up as it flows over it. This increase in airspeed over the top of the airfoil results in a lowering of the pressure and it is that pressure differential between the top and the bottom of the airfoil that is known as lift. However, while the shape of the top of the wing is what generates lift, the force itself is applied to the lower part of the wing, hence the airfoil rises. I guess the best answer would be to say it is produced by the upper part of the airfoil and is applied to the lower part of the airfoil. Look up Bernoulli for a more detailed discussion.

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14y ago
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1mo ago

The upper part of the wing generally produces more lift than the lower part. This is due to the shape of the wing (airfoil) which is designed to create lower pressure above the wing and higher pressure below, resulting in lift.

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Q: Which part of the wing produces more lift the upper part or the lower part?
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How does speed effect lift?

An increase in speed typically leads to an increase in lift generated by an airfoil. This is because higher speeds result in a higher pressure difference between the upper and lower surfaces of the wing, which in turn creates more lift. However, excessive speed can also lead to aerodynamic stalls or other issues that may reduce lift.


What properties of air affect lift?

The properties of air that affect lift include its density (less dense air generates more lift), temperature (warmer air is less dense and can affect lift), pressure (lower pressure can decrease lift), and humidity (moist air is less dense and can reduce lift).


How does extending the wing flaps effect lift and drag?

Extending the wing flaps increases the wing surface area, which can increase lift at lower speeds by creating more lift-producing air pressure. However, the increased surface area also increases drag by creating more drag-inducing air resistance. Overall, extending wing flaps is a trade-off between increasing lift for lower speeds and increasing drag, which can impact fuel efficiency and performance.


Why more lift is required when landing?

More lift is required during landing to counteract the effects of gravity and slow down the aircraft for a safe touch down. By increasing lift, the plane can descend at a controlled rate and reduce its speed gradually without descending too quickly, ensuring a smooth and safe landing.


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How does speed effect lift?

An increase in speed typically leads to an increase in lift generated by an airfoil. This is because higher speeds result in a higher pressure difference between the upper and lower surfaces of the wing, which in turn creates more lift. However, excessive speed can also lead to aerodynamic stalls or other issues that may reduce lift.


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