Dynamic pressure is the pressure exerted by a fluid in motion, which is calculated using the formula $$q = \frac{1}{2} \rho V^2$$, where $$q$$ represents dynamic pressure, $$\rho$$ is the fluid density, and $$V$$ is the flow velocity. This concept is essential in understanding how lift and drag are generated on an airfoil. As air moves over a surface, dynamic pressure influences the behavior of airflow and the forces acting on an aircraft, thus playing a crucial role in aerodynamics.
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