Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 200+ more calculators!
Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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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 chord length for given stick force
Elevator chord=Stick Force/(Gearing ratio*Hinge moment coefficient*0.5*Density*(Velocity^2)*Elevator area) GO

Elevator chord length for given hinge moment coefficient Formula

Elevator chord=Hinge moment/(Hinge moment coefficient*0.5*Density*(Velocity^2)*Elevator area)
c<sub>e</sub>=𝑯<sub>𝒆</sub>/(C<sub>h<sub>e</sub></sub>*0.5*ρ*(v^2)*S<sub>e</sub>)
More formulas
Elevator Hinge moment coefficient GO
Elevator Hinge moment for given hinge moment coefficient GO
Flight velocity for given elevator hinge moment coefficient GO
Elevator area for given hinge moment coefficient GO

What is wing flutter?

The wing flutter is a dynamic instability of a flight vehicle associated with the interaction of aerodynamic, elastic, and inertial forces (aeroelastic phenomena).

How to Calculate Elevator chord length for given hinge moment coefficient?

Elevator chord length for given hinge moment coefficient calculator uses Elevator chord=Hinge moment/(Hinge moment coefficient*0.5*Density*(Velocity^2)*Elevator area) to calculate the Elevator chord, The Elevator chord length for given hinge moment coefficient depends on the elevator hinge moment, area, flight altitude, and velocity. Elevator chord and is denoted by ce symbol.

How to calculate Elevator chord length for given hinge moment coefficient using this online calculator? To use this online calculator for Elevator chord length for given hinge moment coefficient, enter Hinge moment (𝑯𝒆), Hinge moment coefficient (Che), Density (ρ), Velocity (v) and Elevator area (Se) and hit the calculate button. Here is how the Elevator chord length for given hinge moment coefficient calculation can be explained with given input values -> 1.023E-6 = 1.4/(0.77*0.5*997*(60^2)*0.99).

FAQ

What is Elevator chord length for given hinge moment coefficient?
The Elevator chord length for given hinge moment coefficient depends on the elevator hinge moment, area, flight altitude, and velocity and is represented as ce=𝑯𝒆/(Che*0.5*ρ*(v^2)*Se) or Elevator chord=Hinge moment/(Hinge moment coefficient*0.5*Density*(Velocity^2)*Elevator area). Hinge moment is the moment acting on a control surface that the pilot must overcome by exerting a force on the control stick, Hinge moment coefficient is the coefficient associated with the hinge moment of the control surface 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). and The Elevator area is the area of the control surface responsible for providing pitching motion to an aircraft.
How to calculate Elevator chord length for given hinge moment coefficient?
The Elevator chord length for given hinge moment coefficient depends on the elevator hinge moment, area, flight altitude, and velocity is calculated using Elevator chord=Hinge moment/(Hinge moment coefficient*0.5*Density*(Velocity^2)*Elevator area). To calculate Elevator chord length for given hinge moment coefficient, you need Hinge moment (𝑯𝒆), Hinge moment coefficient (Che), Density (ρ), Velocity (v) and Elevator area (Se). With our tool, you need to enter the respective value for Hinge moment, Hinge moment coefficient, Density, Velocity 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 Elevator chord?
In this formula, Elevator chord uses Hinge moment, Hinge moment coefficient, Density, Velocity and Elevator area. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Elevator chord=Stick Force/(Gearing ratio*Hinge moment coefficient*0.5*Density*(Velocity^2)*Elevator area)
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