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D p = ∮ p n ⋅ i d S , Y = ∮ p n ⋅ j d S . displaystyle get started aligned D_ p &=oint pmathbf n cdot mathbf i ;mathrm d S,Y&=oint pmathbf n cdot mathbf j ;mathrm d S.conclude aligned The lift produced by a traditional airfoil is dictated by both equally its design and also the flight situations, for example ahead velocity, angle of attack