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Bernoullis TheoremStatic pressure(P) + Dynamic Pressure(V)= a constant

P+V=K

PV= K

P+V=K

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Bernoullis Theorem

V = KP

LIFT

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Change in Camber(Curvature)

Camber Line

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Angle of Attack

Chord LineAngle of Attack

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Primary Effects

PitchLateral Axis

Elevator

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Primary Effects

YawNormal Axis

Rudder

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Control Functioning

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