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why does drag produce lift?
FredGarvin said:It's the other way around. Lift produces drag. Wellllll...I guess it depends on how you look at it I guess.
I recommend sittting back for an hour or so and read this thread:
https://www.physicsforums.com/showthread.php?t=68355
Care to fill us in as to which ones are incorrect?Antiphon said:Actually, that thread is filled with a lot of consfusing ideas, some of which are actually correct.
If you believe that lift is solely generated by the pressure differential then you didn't read that thread. There are other, more predominant aspects that produce lift, i.e. fully symmetrical airfoils.Antiphon said:Lift is the force on a wing (hopefully upward) which is created by the fact that the pressure above the wing is lower than the pressure below it.
FredGarvin said:Care to fill us in as to which ones are incorrect?
If you believe that lift is solely generated by the pressure differential then you didn't read that thread. There are other, more predominant aspects that produce lift, i.e. fully symmetrical airfoils.
Drag produces lift because of the difference in pressure between the upper and lower surfaces of an airfoil. As air flows over the curved upper surface of an airfoil, it speeds up and creates an area of low pressure. At the same time, the air flowing under the airfoil moves slower, creating an area of high pressure. This pressure difference creates a lifting force, known as lift.
The shape of an airfoil plays a crucial role in producing lift. A curved, asymmetrical airfoil shape is able to create a larger pressure difference between the upper and lower surfaces, resulting in more lift. On the other hand, a flat or symmetrical airfoil is not able to create as much lift.
In addition to airfoil shape, other factors that contribute to lift include the angle of attack (the angle at which the airfoil meets the oncoming air), air density, airspeed, and the size of the airfoil. These factors can all affect the amount of lift produced by an airfoil.
No, drag cannot produce lift on its own. Drag and lift are two separate forces that act on an airfoil. Drag is the force that opposes the motion of an airfoil, while lift is the force that acts perpendicular to the motion of an airfoil. While drag may contribute to the overall aerodynamics of an airfoil, it does not produce lift on its own.
The design of an airfoil can greatly impact the amount of drag it produces. A smooth, streamlined airfoil shape is able to minimize drag and improve the overall aerodynamics of an aircraft. On the other hand, a bulky or poorly designed airfoil can create more drag, which can negatively affect the performance and efficiency of an aircraft.