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Aircraft Mechanics
Lift Coefficient in Static Stability and Control Formulas
lift coefficient is a dimensionless quantity that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity, and an associated reference area. And is denoted by dCl.
Static Stability and Control formulas that make use of Lift Coefficient
f
x
Rudder Deflection Angle given Yawing Moment Coefficient
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FAQ
What is the Lift Coefficient?
lift coefficient is a dimensionless quantity that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity, and an associated reference area.
Can the Lift Coefficient be negative?
{YesorNo}, the Lift Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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