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Aircraft Mechanics
Lift Coefficient in Maneuvering Flight 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 Maneuvering Flight
f
x
Lift Coefficient for given Turn Radius
Go
f
x
Lift Coefficient for given Turn Rate
Go
f
x
Lift Coefficient for given wing loading and turn radius
Go
Maneuvering Flight formulas that make use of Lift Coefficient
f
x
Radius of Turn for given Lift Coefficient
Go
f
x
Turn Rate for given Lift Coefficient
Go
f
x
Radius of Turn for given Wing Loading
Go
f
x
Wing Loading for given Turn Radius
Go
f
x
Turn Rate for given Wing Loading
Go
f
x
Wing Loading for given Turn Rate
Go
f
x
Minimum Flight Velocity
Go
List of variables in Maneuvering Flight formulas
f
x
Aircraft Weight
Go
f
x
Freestream Density
Go
f
x
Reference Area
Go
f
x
Turn Radius
Go
f
x
Turn Rate
Go
f
x
Load Factor
Go
f
x
Wing Loading
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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