What causes a lifting force on an airplane's wing design?

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The lifting force on an airplane's wing is primarily due to the difference in air pressure between the upper and lower surfaces, which can occur even with a thin, flat wing at an angle of attack. The image referenced in the discussion illustrates wing deflection and stresses under load rather than the mechanism of lift generation. It is clarified that the upper and lower surfaces of a thin wing do not need to be curved to produce lift, contradicting common misconceptions. The discussion emphasizes that lift and downward airflow deflection coexist, impacting wing performance. Understanding these principles is essential for grasping how wing design influences flight dynamics.
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As I know, lifting force is because the surface of upper side of the airfoil is longer than the bottom side, causing the pressure of down side larger and produce lefting force...
this is a picture from my lecture notes, which the instructor didn't explained but seems contradict to what I knew...
Anything wrong with my mindset? can anyone help to explain the picture?
Thanks.
 

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There's no contradiction.
The image is nothing to do with how a wing generates lift, it shows deflection and stresses due to a distributed load (which happens to come from the lift force).
You'll find many similar (albeit mostly upside down) images if you google 'beam deflection'.
 
A lifting force coexists with downwards deflection of the air flow relative to the wing. In the case of a thin wing, the upper and lower surfaces have the same length, and they don't need to be curved. A thin flat wing at some angle of attack can generate lift (at the cost of increased drag compared to more efficient wing shapes).

As posted by billy_joule, the image shows an exaggerated example of a wing flexing under load, as viewed from behind (or in front) of an aircraft.
 
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