Dynamic Pressure at Wing for given Vertical Tail Efficiency Calculator

✖Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft.ⓘ Vertical Tail Dynamic Pressure [Q_v]			+10% -10%
✖Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.ⓘ Vertical Tail Efficiency [η_v]			+10% -10%

✖Wing Dynamic Pressure is the dynamic pressure associated with the wing of an aircraft.ⓘ Dynamic Pressure at Wing for given Vertical Tail Efficiency [Q_w]

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Dynamic Pressure at Wing for given Vertical Tail Efficiency Solution

STEP 0: Pre-Calculation Summary

Formula Used

Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency
Q_w = Q_v/η_v
This formula uses 3 Variables

Variables Used

Wing Dynamic Pressure - (Measured in Pascal) - Wing Dynamic Pressure is the dynamic pressure associated with the wing of an aircraft.
Vertical Tail Dynamic Pressure - (Measured in Pascal) - Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft.
Vertical Tail Efficiency - Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.

STEP 1: Convert Input(s) to Base Unit

Vertical Tail Dynamic Pressure: 11 Pascal --> 11 Pascal No Conversion Required
Vertical Tail Efficiency: 16.66 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

Q_w = Q_v/η_v --> 11/16.66

Evaluating ... ...

Q_w = 0.660264105642257

STEP 3: Convert Result to Output's Unit

0.660264105642257 Pascal --> No Conversion Required

FINAL ANSWER

0.660264105642257 ≈ 0.660264 Pascal <-- Wing Dynamic Pressure

(Calculation completed in 00.007 seconds)

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Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has verified this Calculator and 200+ more calculators!

< Wing Tail Interaction Calculators

Wingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle

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

Wing Dynamic Pressure for given Yawing Moment Coefficient

LaTeX Go Wing Dynamic Pressure = Vertical Tail Moment/(Yawing Moment Coefficient*Reference Area*Wingspan)

Wing Area for given Moment Produced by Vertical Tail

LaTeX Go Reference Area = Vertical Tail Moment/(Yawing Moment Coefficient*Wing Dynamic Pressure*Wingspan)

Wingspan for given Yawing Moment Coefficient

LaTeX Go Wingspan = Vertical Tail Moment/(Yawing Moment Coefficient*Reference Area*Wing Dynamic Pressure)

Dynamic Pressure at Wing for given Vertical Tail Efficiency Formula

LaTeX Go

Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency
Q_w = Q_v/η_v

Can a plane fly without a tail?

A tailless aircraft has no tail assembly and no other horizontal surface besides its main wing. The aerodynamic control and stabilization functions in both pitch and roll are incorporated into the main wing. A tailless type may still have a conventional vertical fin (vertical stabilizer) and rudder.

How to Calculate Dynamic Pressure at Wing for given Vertical Tail Efficiency?

Dynamic Pressure at Wing for given Vertical Tail Efficiency calculator uses Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency to calculate the Wing Dynamic Pressure, Dynamic Pressure at Wing for given Vertical Tail Efficiency is the measure of the pressure exerted on an aircraft's wing, calculated by dividing the vertical tail's dynamic pressure by its efficiency, which determines the wing's ability to generate lift and stability during flight. Wing Dynamic Pressure is denoted by Q_w symbol.

How to calculate Dynamic Pressure at Wing for given Vertical Tail Efficiency using this online calculator? To use this online calculator for Dynamic Pressure at Wing for given Vertical Tail Efficiency, enter Vertical Tail Dynamic Pressure (Q_v) & Vertical Tail Efficiency (η_v) and hit the calculate button. Here is how the Dynamic Pressure at Wing for given Vertical Tail Efficiency calculation can be explained with given input values -> 0.660264 = 11/16.66.

FAQ

What is Dynamic Pressure at Wing for given Vertical Tail Efficiency?

Dynamic Pressure at Wing for given Vertical Tail Efficiency is the measure of the pressure exerted on an aircraft's wing, calculated by dividing the vertical tail's dynamic pressure by its efficiency, which determines the wing's ability to generate lift and stability during flight and is represented as Q_w = Q_v/η_v or Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency. Vertical Tail Dynamic Pressure is the dynamic pressure associated with the vertical tail of an aircraft & Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.

How to calculate Dynamic Pressure at Wing for given Vertical Tail Efficiency?

Dynamic Pressure at Wing for given Vertical Tail Efficiency is the measure of the pressure exerted on an aircraft's wing, calculated by dividing the vertical tail's dynamic pressure by its efficiency, which determines the wing's ability to generate lift and stability during flight is calculated using Wing Dynamic Pressure = Vertical Tail Dynamic Pressure/Vertical Tail Efficiency. To calculate Dynamic Pressure at Wing for given Vertical Tail Efficiency, you need Vertical Tail Dynamic Pressure (Q_v) & Vertical Tail Efficiency (η_v). With our tool, you need to enter the respective value for Vertical Tail Dynamic Pressure & Vertical Tail Efficiency and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Wing Dynamic Pressure?

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

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

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