Lift coefficient
Input(s)
\(\rho\): Density \(\left(\mathrm{kg} / \mathrm{m}^{3}\right)\)
v: True Air Speed \((\mathrm{m} / \mathrm{s})\).
L: Lift Force (Newton)
S: Planform Area \(\left(\mathrm{m}^{2}\right)\)
Output(s)
\(C_{L}\): Lift Coefficient (dimensionless)
Formula(s)
\[
\mathrm{C}_{\mathrm{L}}=2 * \frac{\mathrm{L}}{\rho * \mathrm{v}^{2} * \mathrm{~S}}
\]
Reference(s)
Wikipedia.org.