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Aircraft Mechanics
Vertical Tail Dynamic Pressure in Directional Stability Formulas
Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft. And is denoted by Q
v
. Vertical Tail Dynamic Pressure is usually measured using the Pascal for Pressure. Note that the value of Vertical Tail Dynamic Pressure is always positive.
Formulas to find Vertical Tail Dynamic Pressure in Directional Stability
f
x
Vertical Tail Dynamic Pressure for given Vertical Tail Side Force
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
Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency
Go
Directional Stability formulas that make use of Vertical Tail Dynamic Pressure
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Vertical Tail Angle of Attack 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 Lift Curve Slope for Given Moment
Go
f
x
Vertical Tail Moment Arm for Given Yawing Moment Coefficient
Go
f
x
Vertical Tail Efficiency
Go
f
x
Vertical Tail Area for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Lift Curve Slope 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
Wing Area for given Yawing Moment Coefficient
Go
f
x
Dynamic Pressure at Wing for given Vertical Tail Efficiency
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
List of variables in Directional Stability formulas
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Vertical Tail Angle of Attack
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
Reference Area
Go
f
x
Wingspan
Go
f
x
Wing Dynamic Pressure
Go
f
x
Vertical Tail Efficiency
Go
FAQ
What is the Vertical Tail Dynamic Pressure?
Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft. Vertical Tail Dynamic Pressure is usually measured using the Pascal for Pressure. Note that the value of Vertical Tail Dynamic Pressure is always positive.
Can the Vertical Tail Dynamic Pressure be negative?
No, the Vertical Tail Dynamic Pressure, measured in Pressure cannot be negative.
What unit is used to measure Vertical Tail Dynamic Pressure?
Vertical Tail Dynamic Pressure is usually measured using the Pascal[Pa] for Pressure. Kilopascal[Pa], Bar[Pa], Pound Per Square Inch[Pa] are the few other units in which Vertical Tail Dynamic Pressure can be measured.
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