Dynamic Pressure at Vertical Tail in Static Stability and Control Formulas

The Dynamic Pressure at Vertical Tail of an aircraft is the pressure exerted by the air flowing past the tail due to the aircraft’s forward motion. And is denoted by Q_v. Dynamic Pressure at Vertical Tail is usually measured using the Pascal for Pressure. Note that the value of Dynamic Pressure at Vertical Tail is always negative.

Static Stability and Control formulas that make use of Dynamic Pressure at Vertical Tail

fxYawing Moment Coefficient given Rudder DeflectionGo

fxRudder Deflection Angle given Yawing Moment CoefficientGo

FAQ

What is the Dynamic Pressure at Vertical Tail?

The Dynamic Pressure at Vertical Tail of an aircraft is the pressure exerted by the air flowing past the tail due to the aircraft’s forward motion. Dynamic Pressure at Vertical Tail is usually measured using the Pascal for Pressure. Note that the value of Dynamic Pressure at Vertical Tail is always negative.

Can the Dynamic Pressure at Vertical Tail be negative?

Yes, the Dynamic Pressure at Vertical Tail, measured in Pressure can be negative.

What unit is used to measure Dynamic Pressure at Vertical Tail?

Dynamic Pressure at Vertical Tail 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 Dynamic Pressure at Vertical Tail can be measured.

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