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From: Who says "Nothing is impossible" ? I've been doing nothing for years.
It's just kinda funny, was taught this in school and been thinking this way for 30 years, then all of sudden you learn different. The theory I was taught was the wing was longer at the top making the air pass over the top faster to reach the back at the same time the air going under the bottom does. Who says the air has to meet at the back of the wing at the same time ?
Allot of unproven theory and bs out there you have to watch it
It's just kinda funny, was taught this in school and been thinking this way for 30 years, then all of sudden you learn different. The theory I was taught was the wing was longer at the top making the air pass over the top faster to reach the back at the same time the air going under the bottom does. Who says the air has to meet at the back of the wing at the same time ?
Allot of unproven theory and bs out there you have to watch it
well, if you think about the wing displacing the (*relatively* unmoving) air molecules at the stagnation point and then moving one upward while passing through, you can see how, negating skin friction, the molecules *would* meet at the back. you have to think of it as a wing moving through air, though.
It's just kinda funny, was taught this in school and been thinking this way for 30 years, then all of sudden you learn different. Allot of unproven theory and bs out there you have to watch it
The Kutta condition is the mathematical theory you are referring to. It basically says the flow over the upper and lower surfaces of the airfoil meet at the same time.
At low angles of attack, the flow over the upper and lower surfaces do meet at the trailing edge at the same time. However, at higher angles of attack the Kutta condition breaks down. See this NASA high angle of attack airfoil flow visualization:
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