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Aircraft Mechanics
Lift Coefficient Roll Control in Static Stability and Control Formulas
The Lift Coefficient Roll Control is a dimensionless quantity that shows how much lift a lifting body creates relative to the fluid density, velocity, and an associated reference area. And is denoted by C
l
.
Formulas to find Lift Coefficient Roll Control in Static Stability and Control
f
x
Aileron Section lift Coefficient given Aileron Deflection
Go
f
x
Aileron Deflection given Aileron Lift Coefficient
Go
f
x
Aileron Section Lift Coefficient given Control Effectiveness
Go
Static Stability and Control formulas that make use of Lift Coefficient Roll Control
f
x
Aileron Control Effectiveness given Aileron Deflection
Go
f
x
Deflection Angle given Lift Coefficient
Go
f
x
Lift Coefficient Slope Roll Control
Go
List of variables in Static Stability and Control formulas
f
x
Lift Coefficient Slope Roll Control
Go
f
x
Rate of change of Angle of Attack
Go
f
x
Rate of change of Deflection of Aileron
Go
f
x
Deflection of Aileron
Go
f
x
Derivative of Wing Lift Coefficient
Go
f
x
Flap Effectiveness Parameter
Go
f
x
Wing Area
Go
f
x
Wingspan
Go
f
x
Chord
Go
f
x
Initial Length
Go
f
x
Final Length
Go
FAQ
What is the Lift Coefficient Roll Control?
The Lift Coefficient Roll Control is a dimensionless quantity that shows how much lift a lifting body creates relative to the fluid density, velocity, and an associated reference area.
Can the Lift Coefficient Roll Control be negative?
{YesorNo}, the Lift Coefficient Roll Control, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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