Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency Calculator

Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency is a measure of the pressure exerted by the air flowing over the vertical tail of an aircraft, influenced by the efficiency of the vertical tail and the dynamic pressure of the wing, it is an important factor in determining the stability and control of the aircraft during flight, the formula calculates this pressure based on the vertical tail efficiency and wing dynamic pressure, providing a critical input for aircraft design and performance analysis is calculated using Vertical Tail Dynamic Pressure = Vertical Tail Efficiency*Wing Dynamic Pressure. To calculate Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency, you need Vertical Tail Efficiency (η_v) & Wing Dynamic Pressure (Q_w). With our tool, you need to enter the respective value for Vertical Tail Efficiency & Wing Dynamic Pressure and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

In this formula, Vertical Tail Dynamic Pressure uses Vertical Tail Efficiency & Wing Dynamic Pressure. We can use 2 other way(s) to calculate the same, which is/are as follows -

• Vertical Tail Dynamic Pressure = Vertical Tail Moment/(Vertical Tail Moment Arm*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle)*Vertical Tail Area)
• Vertical Tail Dynamic Pressure = Yawing Moment Coefficient*Reference Area*Wingspan*Wing Dynamic Pressure/(Vertical Tail Moment Arm*Vertical Tail Area*Vertical Tail Lift Curve Slope*(Sideslip Angle+Sidewash Angle))