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Aircraft Mechanics
Vertical Tail Lift Curve Slope in Directional Stability Formulas
The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft. And is denoted by C
v
. Vertical Tail Lift Curve Slope is usually measured using the 1 per Radian for Reciprocal Angle. Note that the value of Vertical Tail Lift Curve Slope is always negative.
Formulas to find Vertical Tail Lift Curve Slope in Directional Stability
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Vertical Tail Lift Curve Slope for Given Moment
Go
f
x
Vertical Tail Lift Curve Slope for given Vertical Tail Efficiency
Go
f
x
Vertical Tail Lift Curve Slope for given Yawing Moment Coefficient
Go
Directional Stability formulas that make use of Vertical Tail Lift Curve Slope
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Angle of Attack for given Vertical Tail Side Force
Go
f
x
Vertical Tail Dynamic Pressure for given Vertical Tail Side Force
Go
f
x
Vertical Tail Area for given Vertical Tail Side Force
Go
f
x
Moment Produced by Vertical Tail for given Lift Curve Slope
Go
f
x
Vertical Tail Moment Arm for given Lift Curve Slope
Go
f
x
Vertical Tail Moment Arm for Given Yawing Moment Coefficient
Go
f
x
Vertical Tail Volume Ratio for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Efficiency for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Area for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Area for given Moment
Go
f
x
Wingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle
Go
f
x
Dynamic Pressure at Wing for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Dynamic Pressure for given Moment
Go
f
x
Dynamic Pressure at Vertical Tail for given Yawing Moment Coefficient
Go
f
x
Wing Area for given Yawing Moment Coefficient
Go
f
x
Sidewash Angle for given Moment Produced by Vertical Tail
Go
f
x
Yawing Moment Coefficient for given Vertical Tail Lift Curve Slope
Go
f
x
Sideslip Angle for given Moment Produced by Vertical Tail
Go
f
x
SideSlip Angle for given Yawing Moment Coefficient
Go
f
x
Sidewash Angle given Yawing Moment Coefficient using Wingspan
Go
f
x
Yawing Moment Coefficient for given Vertical Tail Volume Ratio
Go
f
x
Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency
Go
f
x
Sidewash Angle for given Yawing Moment Coefficient
Go
List of variables in Directional Stability formulas
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Angle of Attack
Go
f
x
Vertical Tail Dynamic Pressure
Go
f
x
Vertical Tail Area
Go
f
x
Vertical Tail Moment
Go
f
x
Vertical Tail Moment Arm
Go
f
x
Sideslip Angle
Go
f
x
Sidewash Angle
Go
f
x
Yawing Moment Coefficient
Go
f
x
Vertical Tail Volume Ratio
Go
f
x
Vertical Tail Efficiency
Go
f
x
Reference Area
Go
f
x
Wingspan
Go
f
x
Wing Dynamic Pressure
Go
FAQ
What is the Vertical Tail Lift Curve Slope?
The Vertical Tail Lift Curve Slope is the slope associated with the lift curve of a vertical tailplane of an aircraft. Vertical Tail Lift Curve Slope is usually measured using the 1 per Radian for Reciprocal Angle. Note that the value of Vertical Tail Lift Curve Slope is always negative.
Can the Vertical Tail Lift Curve Slope be negative?
Yes, the Vertical Tail Lift Curve Slope, measured in Reciprocal Angle can be negative.
What unit is used to measure Vertical Tail Lift Curve Slope?
Vertical Tail Lift Curve Slope is usually measured using the 1 per Radian[rad⁻¹] for Reciprocal Angle. 1 per Degree[rad⁻¹], 1 per Minute[rad⁻¹], 1 per Quadrant[rad⁻¹] are the few other units in which Vertical Tail Lift Curve Slope can be measured.
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