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Aircraft Mechanics
Lift Coefficient in Longitudinal Stability Formulas
The Lift Coefficient is a dimensionless coefficient 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 C
L
.
Formulas to find Lift Coefficient in Longitudinal Stability
f
x
Total Lift Coefficient of Wing-Tail Combination
Go
Longitudinal Stability formulas that make use of Lift Coefficient
f
x
Wing Lift Coefficient of wing-tail combination
Go
f
x
Tail Lift Coefficient of Wing-Tail Combination
Go
f
x
Tail Efficiency for given lift coefficients
Go
f
x
Tail area for given tail efficiency
Go
List of variables in Longitudinal Stability formulas
f
x
Wing Lift Coefficient
Go
f
x
Tail Efficiency
Go
f
x
Horizontal Tail Area
Go
f
x
Tail Lift Coefficient
Go
f
x
Reference Area
Go
FAQ
What is the Lift Coefficient?
The Lift Coefficient is a dimensionless coefficient 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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