how centre of pressure on an aerofoil varies with angle of attack
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So, Thé ÃnSwer is --) The center of pressure on a symmetricairfoil typically lies close to 25% of the chord length behind the leading edge of the airfoil. (This is called the "quarter-chord point".) For a symmetricairfoil, as angle of attack and lift coefficient change, the center of pressure does not move.
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So, Thé ÃnSwer is --) The center of pressure on a symmetricairfoil typically lies close to 25% of the chord length behind the leading edge of the airfoil. (This is called the "quarter-chord point".) For a symmetricairfoil, as angle of attack and lift coefficient change, the center of pressure does not move.
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