Hinge moment coefficient for given stick force Calculator

Category	Physics ↺
Physics	Flight Stability and Control ↺
Flight-Stability-And-Control	Static Stability and Control ↺
Static-Stability-And-Control	Stick Forces ↺
Stick-Forces	Relationship between Stick Force and Hinge Moment ↺

✖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%
✖The density of a material shows the denseness of that material in a specific given area. This is taken as mass per unit volume of a given object. ⓘ Density [ρ]			+10% -10%
✖Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). ⓘ Velocity [v]			+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%
✖The Elevator area is the area of the control surface responsible for providing pitching motion to an aircraftⓘ Elevator area [S_e]			+10% -10%

✖Hinge moment coefficient is the coefficient associated with the hinge moment of the control surface of an aircraftⓘ Hinge moment coefficient for given stick force [C_{h_e}]

⎘ Copy

👎 Report Issue!

👍 Share Now!

You are here:

Vinay Mishra

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

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

Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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

< 11 Other formulas that you can solve using the same Inputs

Stanton Number (using basic fluid properties)

Stanton Number=External convection heat transfer coefficient/(Specific Heat Capacity*Fluid Velocity*Density) GO

Reynolds Number for Non-Circular Tubes

Reynolds Number=Density*Fluid Velocity*Characteristic Length/Dynamic viscosity GO

Reynolds Number for Circular Tubes

Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO

Air Resistance Force

Air Resistance=Air Constant*Velocity^2 GO

Archimedes Principle

Archimedes Principle=Density*Acceleration Due To Gravity*Velocity GO

Pressure when density and height are given

Pressure=Density*Acceleration Due To Gravity*Height GO

Molar Volume

Molar Volume=(Atomic Weight*Molar Mass)/Density GO

Centripetal Force

Centripetal Force=(Mass*(Velocity)^2)/Radius GO

Number of atomic sites

Number of atomic sites=Density/Atomic Mass GO

Relative Density

Relative Density=Density/Water Density GO

Kinetic Energy

Kinetic Energy=(Mass*Velocity^2)/2 GO

< 1 Other formulas that calculate the same Output

Elevator Hinge moment coefficient

Hinge moment coefficient=Hinge moment/(0.5*Density*(Velocity^2)*Elevator area*Elevator chord) GO

Hinge moment coefficient for given stick force Formula

Hinge moment coefficient=Stick Force/(Gearing ratio*0.5*Density*(Velocity^2)*Elevator chord*Elevator area)
Che=𝙁/(𝑮*0.5*ρ*(v^2)*ce*Se)

More formulas

Elevator Stick Force GO

Stick length for given stick force GO

Stick deflection angle for given stick force GO

Hinge moment for given stick force GO

Elevator deflection angle for given stick force GO

Elevator Stick force for given gearing ratio GO

Gearing ratio for given stick force GO

Hinge moment for given gearing ratio GO

Gearing ratio GO

Elevator deflection angle for given gearing ratio GO

Control stick length for given gearing ratio GO

Stick deflection angle for given gearing ratio GO

Elevator stick force for given hinge moment coefficient GO

Gearing ratio for given hinge moment coefficient GO

Flight velocity for given stick force GO

Elevator area for given stick force GO

Elevator chord length for given stick force GO

Why do aircraft control surfaces need balancing?

When an aircraft is repainted, the balance of the control surfaces must be checked. Any control surface out of balance is unstable and does not remain in a streamlined position during normal flight.

How to Calculate Hinge moment coefficient for given stick force?

Hinge moment coefficient for given stick force calculator uses Hinge moment coefficient=Stick Force/(Gearing ratio*0.5*Density*(Velocity^2)*Elevator chord*Elevator area) to calculate the Hinge moment coefficient, The Hinge moment coefficient for given stick force is a function of the control system's gearing ratio, elevator chord, area, flight altitude, and velocity. Hinge moment coefficient and is denoted by C_{h_e} symbol.

How to calculate Hinge moment coefficient for given stick force using this online calculator? To use this online calculator for Hinge moment coefficient for given stick force, enter Stick Force (𝙁), Gearing ratio (𝑮), Density (ρ), Velocity (v), Elevator chord (c_e) and Elevator area (S_e) and hit the calculate button. Here is how the Hinge moment coefficient for given stick force calculation can be explained with given input values -> 2.017E-6 = 2/(0.93*0.5*997*(60^2)*0.6*0.99).

FAQ

What is Hinge moment coefficient for given stick force?

The Hinge moment coefficient for given stick force is a function of the control system's gearing ratio, elevator chord, area, flight altitude, and velocity and is represented as C_{h_e}=𝙁/(𝑮*0.5*ρ*(v^2)*c_e*S_e) or Hinge moment coefficient=Stick Force/(Gearing ratio*0.5*Density*(Velocity^2)*Elevator chord*Elevator area). 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, The density of a material shows the denseness of that material in a specific given area. This is taken as mass per unit volume of a given object. , Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). , Elevator chord is the chord length of an elevator measured from its hinge line to trailing edge and The Elevator area is the area of the control surface responsible for providing pitching motion to an aircraft.

How to calculate Hinge moment coefficient for given stick force?

The Hinge moment coefficient for given stick force is a function of the control system's gearing ratio, elevator chord, area, flight altitude, and velocity is calculated using Hinge moment coefficient=Stick Force/(Gearing ratio*0.5*Density*(Velocity^2)*Elevator chord*Elevator area). To calculate Hinge moment coefficient for given stick force, you need Stick Force (𝙁), Gearing ratio (𝑮), Density (ρ), Velocity (v), Elevator chord (c_e) and Elevator area (S_e). With our tool, you need to enter the respective value for Stick Force, Gearing ratio, Density, Velocity, Elevator chord and Elevator area 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 Hinge moment coefficient?

In this formula, Hinge moment coefficient uses Stick Force, Gearing ratio, Density, Velocity, Elevator chord and Elevator area. We can use 1 other way(s) to calculate the same, which is/are as follows -

Hinge moment coefficient=Hinge moment/(0.5*Density*(Velocity^2)*Elevator area*Elevator chord)

Facebook
Twitter
WhatsApp
Reddit
LinkedIn
E-Mail

Let Others Know

✖

Facebook

Twitter

Copied!