[Physics] Position of aerofoil force moment, center of pressure, aerodynamic center

aerodynamics

I'm confused by wikipedia's page on aerofoils, the aerodynamic center, and center of pressure; it seems to contradict itself.

The airofoils page says the center of pressure is at the same position as the aerodynamic center. It says they are both the position on the wing where the moment is zero, and that they are one quarter of the chord length from the leading edge.

Yet the Aerodynamic center page says:

For non-symmetric (cambered) airfoils the quarter-chord is only an
approximation for the aerodynamic center.

And the center of pressure page says:

The location of the center of pressure varies with changes of lift
coefficient and angle of attack.

I would appreciate an explanation of the difference between center of pressure and aerodynamic center – e.g. are they both the point at which there is no moment? What's the difference between the two? Please keep terminology as close to layman's terms as possible, particularly as little maths as possible.

Thanks!

Best Answer

I think I've found the answer. On the pitching moment page it says:

The aerodynamic center is defined to be the point on the chord line of the airfoil at which the pitching moment coefficient does not vary with angle of attack,[2] or at least does not vary significantly over the operating range of angle of attack of the airfoil.

However the question remains, what is the position of the aerodynamic centre and centre of pressure?

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