Flight Velocity for given Stick Force Calculator

✖Stick Force is the force exerted on the control column by the pilot of an airplane in flight.ⓘ Stick Force [𝙁]			+10% -10%
✖Gearing Ratio is a measure of the mechanical advantage provided by the control system of an aircraft.ⓘ Gearing Ratio [𝑮]			+10% -10%
✖Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft.ⓘ Hinge Moment Coefficient [Ch_e]			+10% -10%
✖Density of flow refers to the mass per unit volume of a fluid through which aircraft is moving.ⓘ Density [ρ]			+10% -10%
✖The Elevator Area is the area of the control surface responsible for providing pitching motion to an aircraft.ⓘ Elevator Area [S_e]			+10% -10%
✖Elevator Chord is the chord length of an elevator measured from its hinge line to trailing edge.ⓘ Elevator Chord [c_e]			+10% -10%

✖Flight Velocity refers to the speed at which an aircraft moves through the air.ⓘ Flight Velocity for given Stick Force [V]

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Flight Velocity for given Stick Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Flight Velocity = sqrt(Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord))
V = sqrt(𝙁/(𝑮*Ch_e*0.5*ρ*S_e*c_e))
This formula uses 1 Functions, 7 Variables

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Flight Velocity - (Measured in Meter per Second) - Flight Velocity refers to the speed at which an aircraft moves through the air.
Stick Force - (Measured in Newton) - Stick Force is the force exerted on the control column by the pilot of an airplane in flight.
Gearing Ratio - (Measured in 1 per Meter) - Gearing Ratio is a measure of the mechanical advantage provided by the control system of an aircraft.
Hinge Moment Coefficient - Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft.
Density - (Measured in Kilogram per Cubic Meter) - Density of flow refers to the mass per unit volume of a fluid through which aircraft is moving.
Elevator Area - (Measured in Square Meter) - The Elevator Area is the area of the control surface responsible for providing pitching motion to an aircraft.
Elevator Chord - (Measured in Meter) - Elevator Chord is the chord length of an elevator measured from its hinge line to trailing edge.

STEP 1: Convert Input(s) to Base Unit

Stick Force: 23.25581 Newton --> 23.25581 Newton No Conversion Required
Gearing Ratio: 0.930233 1 per Meter --> 0.930233 1 per Meter No Conversion Required
Hinge Moment Coefficient: 0.770358 --> No Conversion Required
Density: 1.225 Kilogram per Cubic Meter --> 1.225 Kilogram per Cubic Meter No Conversion Required
Elevator Area: 0.02454 Square Meter --> 0.02454 Square Meter No Conversion Required
Elevator Chord: 0.6 Meter --> 0.6 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V = sqrt(𝙁/(𝑮*Ch_e*0.5*ρ*S_e*c_e)) --> sqrt(23.25581/(0.930233*0.770358*0.5*1.225*0.02454*0.6))

Evaluating ... ...

V = 59.9870651715788

STEP 3: Convert Result to Output's Unit

59.9870651715788 Meter per Second --> No Conversion Required

FINAL ANSWER

59.9870651715788 ≈ 59.98707 Meter per Second <-- Flight Velocity

(Calculation completed in 00.004 seconds)

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Home » Physics » Aircraft Mechanics » Static Stability and Control » Longitudinal Control » Aerospace » Stick Forces and Hinge Moments » Flight Velocity for given Stick Force

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 Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ more calculators!

< Stick Forces and Hinge Moments Calculators

Flight Velocity given Elevator Hinge Moment Coefficient

LaTeX Go Flight Velocity = sqrt(Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord))

Elevator Area given Hinge Moment Coefficient

LaTeX Go Elevator Area = Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord)

Elevator Hinge moment coefficient

LaTeX Go Hinge Moment Coefficient = Hinge Moment/(0.5*Density*Flight Velocity^2*Elevator Area*Elevator Chord)

Elevator Hinge Moment given Hinge Moment Coefficient

LaTeX Go Hinge Moment = Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area*Elevator Chord

Flight Velocity for given Stick Force Formula

LaTeX Go

Flight Velocity = sqrt(Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord))
V = sqrt(𝙁/(𝑮*Ch_e*0.5*ρ*S_e*c_e))

What is Loadsheet?

Loadsheet is a weight & balance data to a particular flight basically containing the weight of passengers, baggage, cargo, etc.

How to Calculate Flight Velocity for given Stick Force?

Flight Velocity for given Stick Force calculator uses Flight Velocity = sqrt(Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord)) to calculate the Flight Velocity, Flight Velocity for Given Stick Force is a measure that calculates the airspeed of an aircraft in response to a specific stick force, taking into account factors such as gearing ratio, hinge moment coefficient, air density, elevator area, and elevator chord. Flight Velocity is denoted by V symbol.

How to calculate Flight Velocity for given Stick Force using this online calculator? To use this online calculator for Flight Velocity for given Stick Force, enter Stick Force (𝙁), Gearing Ratio (𝑮), Hinge Moment Coefficient (Ch_e), Density (ρ), Elevator Area (S_e) & Elevator Chord (c_e) and hit the calculate button. Here is how the Flight Velocity for given Stick Force calculation can be explained with given input values -> 60.00101 = sqrt(23.25581/(0.930233*0.770358*0.5*1.225*0.02454*0.6)).

FAQ

What is Flight Velocity for given Stick Force?

Flight Velocity for Given Stick Force is a measure that calculates the airspeed of an aircraft in response to a specific stick force, taking into account factors such as gearing ratio, hinge moment coefficient, air density, elevator area, and elevator chord and is represented as V = sqrt(𝙁/(𝑮*Ch_e*0.5*ρ*S_e*c_e)) or Flight Velocity = sqrt(Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord)). Stick Force is the force exerted on the control column by the pilot of an airplane in flight, Gearing Ratio is a measure of the mechanical advantage provided by the control system of an aircraft, Hinge Moment Coefficient is the coefficient associated with the hinge moment of the control surface of an aircraft, Density of flow refers to the mass per unit volume of a fluid through which aircraft is moving, The Elevator Area is the area of the control surface responsible for providing pitching motion to an aircraft & Elevator Chord is the chord length of an elevator measured from its hinge line to trailing edge.

How to calculate Flight Velocity for given Stick Force?

Flight Velocity for Given Stick Force is a measure that calculates the airspeed of an aircraft in response to a specific stick force, taking into account factors such as gearing ratio, hinge moment coefficient, air density, elevator area, and elevator chord is calculated using Flight Velocity = sqrt(Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord)). To calculate Flight Velocity for given Stick Force, you need Stick Force (𝙁), Gearing Ratio (𝑮), Hinge Moment Coefficient (Ch_e), Density (ρ), Elevator Area (S_e) & Elevator Chord (c_e). With our tool, you need to enter the respective value for Stick Force, Gearing Ratio, Hinge Moment Coefficient, Density, Elevator Area & Elevator Chord 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 Flight Velocity?

In this formula, Flight Velocity uses Stick Force, Gearing Ratio, Hinge Moment Coefficient, Density, Elevator Area & Elevator Chord. We can use 1 other way(s) to calculate the same, which is/are as follows -

Flight Velocity = sqrt(Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord))

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