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Flight velocity for given elevator hinge moment coefficient Calculator

Category Physics ↺
Physics Flight Stability and Control ↺
Flight-Stability-And-Control Static Stability and Control ↺
Static-Stability-And-Control Longitudinal Control ↺
Longitudinal-Control Elevator Hinge Moment ↺
✖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 [𝑯𝒆]
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✖Hinge moment coefficient is the coefficient associated with the hinge moment of the control surface of an aircraftⓘ Hinge moment coefficient [Che]
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✖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]
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✖The Elevator area is the area of the control surface responsible for providing pitching motion to an aircraftⓘ Elevator area [Se]
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✖Elevator chord is the chord length of an elevator measured from its hinge line to trailing edgeⓘ Elevator chord [ce]
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✖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). ⓘ Flight velocity for given elevator hinge moment coefficient [v]
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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
Thermal Diffusivity
Thermal Diffusivity=Thermal Conductivity/(Density*Specific Heat Capacity) GO
Reynolds Number for Circular Tubes
Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO
Inertial Force Per Unit Area
Inertial Force per unit area=(Fluid Velocity^2)*Density GO
Pressure when density and height are given
Pressure=Density*Acceleration Due To Gravity*Height GO
Turbulence
Turbulence=Density*Dynamic viscosity*Fluid Velocity GO
Molar Volume
Molar Volume=(Atomic Weight*Molar Mass)/Density GO
Momentum Diffusivity
Momentum diffusivity=Dynamic viscosity/Density GO
Number of atomic sites
Number of atomic sites=Density/Atomic Mass GO
Relative Density
Relative Density=Density/Water Density GO

11 Other formulas that calculate the same Output

Velocity of the follower after time t (Cycloidal motion)
Velocity=((Angular velocity of the cam*Stroke of the follower)/Angular displacement of the cam during out stroke)*(1-(cos((2*pi*Angle through which the cam rotates)/(Angular displacement of the cam during out stroke)))) GO
Velocity of the follower for tangent cam with roller follower(contact with straight flanks)
Velocity=Angular velocity of the cam*(Radius of the base circle+Radius of the roller)*(sin(Angle turned by cam from beginning of roller)/((cos(Angle turned by cam from beginning of roller))^2)) GO
Velocity OF A Progressive Wave
Velocity=Wavelength Of A Wave/Time Period Of Progressive Wave GO
Velocity Of The Particle
Velocity=(Quantum Number*Plancks Constant)/(Mass*Radius*2*pi) GO
Velocity due to voltage
Velocity=sqrt((2*[Charge-e]*Velocity of electron)/[Mass-e]) GO
Velocity Of Wave in String
Velocity=sqrt(Tension Of String/Mass Per Unit length) GO
Velocity OF A Progressive Wave(Using Angular Frequency)
Velocity=(Wavelength*Angular Frequency)/(4*pi) GO
Velocity OF A Progressive Wave(Using Frequency)
Velocity=Wavelength Of A Wave*frequency GO
Velocity Of A Wave(Using Wave Number)
Velocity=Angular Frequency/Wave Number GO
Velocity Of Sound In Liquid
Velocity=sqrt(bulk modulus/Density) GO
Velocity Of Sound In Solids
Velocity=sqrt(Elasticity/Density) GO

Flight velocity for given elevator hinge moment coefficient Formula

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

What is flutter?

Flutter is a hazardous condition; if it is not stopped, it can cause structural failure and potentially lead to a fatal accident.

How to Calculate Flight velocity for given elevator hinge moment coefficient?

Flight velocity for given elevator hinge moment coefficient calculator uses Velocity=sqrt(Hinge moment/(Hinge moment coefficient*0.5*Density*Elevator area*Elevator chord)) to calculate the Velocity, The Flight velocity for given elevator hinge moment coefficient is a function of elevator hinge moment, the altitude of flight, elevator area, and chord. Velocity and is denoted by v symbol.

How to calculate Flight velocity for given elevator hinge moment coefficient using this online calculator? To use this online calculator for Flight velocity for given elevator hinge moment coefficient, enter Hinge moment (𝑯𝒆), Hinge moment coefficient (Che), Density (ρ), Elevator area (Se) and Elevator chord (ce) and hit the calculate button. Here is how the Flight velocity for given elevator hinge moment coefficient calculation can be explained with given input values -> 0.07836 = sqrt(1.4/(0.77*0.5*997*0.99*0.6)).

FAQ

What is Flight velocity for given elevator hinge moment coefficient?
The Flight velocity for given elevator hinge moment coefficient is a function of elevator hinge moment, the altitude of flight, elevator area, and chord and is represented as v=sqrt(𝑯𝒆/(Che*0.5*ρ*Se*ce)) or Velocity=sqrt(Hinge moment/(Hinge moment coefficient*0.5*Density*Elevator area*Elevator chord)). 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. , The Elevator area is the area of the control surface responsible for providing pitching motion to an aircraft and Elevator chord is the chord length of an elevator measured from its hinge line to trailing edge.
How to calculate Flight velocity for given elevator hinge moment coefficient?
The Flight velocity for given elevator hinge moment coefficient is a function of elevator hinge moment, the altitude of flight, elevator area, and chord is calculated using Velocity=sqrt(Hinge moment/(Hinge moment coefficient*0.5*Density*Elevator area*Elevator chord)). To calculate Flight velocity for given elevator hinge moment coefficient, you need Hinge moment (𝑯𝒆), Hinge moment coefficient (Che), Density (ρ), Elevator area (Se) and Elevator chord (ce). With our tool, you need to enter the respective value for Hinge moment, Hinge moment coefficient, Density, Elevator area and 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 Velocity?
In this formula, Velocity uses Hinge moment, Hinge moment coefficient, Density, Elevator area and Elevator chord. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Velocity=Wavelength Of A Wave/Time Period Of Progressive Wave
  • Velocity=Wavelength Of A Wave*frequency
  • Velocity=(Wavelength*Angular Frequency)/(4*pi)
  • Velocity=Angular Frequency/Wave Number
  • Velocity=sqrt(Tension Of String/Mass Per Unit length)
  • Velocity=sqrt(bulk modulus/Density)
  • Velocity=sqrt(Elasticity/Density)
  • Velocity=sqrt((2*[Charge-e]*Velocity of electron)/[Mass-e])
  • Velocity=(Quantum Number*Plancks Constant)/(Mass*Radius*2*pi)
  • Velocity=((Angular velocity of the cam*Stroke of the follower)/Angular displacement of the cam during out stroke)*(1-(cos((2*pi*Angle through which the cam rotates)/(Angular displacement of the cam during out stroke))))
  • Velocity=Angular velocity of the cam*(Radius of the base circle+Radius of the roller)*(sin(Angle turned by cam from beginning of roller)/((cos(Angle turned by cam from beginning of roller))^2))
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