The formula for the drag force is given by:
$F_{d} = 0.5 * C_{d} * A * \rho * v^{2}$
where:
- $F_{d}$ is the drag force,
- $C_{d}$ is the drag coefficient,
- $A$ is the frontal area,
- $\rho$ is the air density (which is approximately $1.2 \mathrm{kg/m^{3}}$ at
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