Elevator Area given Stick Force Solution

STEP 0: Pre-Calculation Summary
Formula Used
Elevator Area = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord)
Se = ๐™/(๐‘ฎ*Che*0.5*ฯ*V^2*ce)
This formula uses 7 Variables
Variables Used
Elevator Area - (Measured in Square Meter) - The Elevator area is the area of the control surface responsible for providing pitching motion to an aircraft.
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.
Flight Velocity - (Measured in Meter per Second) - Flight Velocity refers to the speed at which an aircraft moves through the air.
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: 23.25 Newton --> 23.25 Newton No Conversion Required
Gearing Ratio: 0.93 1 per Meter --> 0.93 1 per Meter No Conversion Required
Hinge Moment Coefficient: 0.77 --> No Conversion Required
Density: 1.225 Kilogram per Cubic Meter --> 1.225 Kilogram per Cubic Meter No Conversion Required
Flight Velocity: 60 Meter per Second --> 60 Meter per Second No Conversion Required
Elevator Chord: 0.6 Meter --> 0.6 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Se = ๐™/(๐‘ฎ*Che*0.5*ฯ*V^2*ce) --> 23.25/(0.93*0.77*0.5*1.225*60^2*0.6)
Evaluating ... ...
Se = 0.0245408408673715
STEP 3: Convert Result to Output's Unit
0.0245408408673715 Square Meter --> No Conversion Required
FINAL ANSWER
0.0245408408673715 โ‰ˆ 0.024541 Square Meter <-- Elevator Area
(Calculation completed in 00.004 seconds)

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
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23 Stick Forces and Hinge Moments Calculators

Flight velocity for given stick force
Go Flight Velocity = sqrt(Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord))
Gearing Ratio given Hinge Moment Coefficient
Go Gearing Ratio = Stick Force/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area*Elevator Chord)
Hinge Moment Coefficient given Stick Force
Go Hinge Moment Coefficient = Stick Force/(Gearing Ratio*0.5*Density*Flight Velocity^2*Elevator Chord*Elevator Area)
Elevator Chord Length given Stick Force
Go Elevator Chord = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area)
Elevator Area given Stick Force
Go Elevator Area = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord)
Elevator Stick Force Given Hinge Moment Coefficient
Go Stick Force = Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord*Elevator Area
Flight Velocity given Elevator Hinge Moment Coefficient
Go Flight Velocity = sqrt(Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Elevator Area*Elevator Chord))
Elevator Chord Length given Hinge Moment Coefficient
Go Elevator Chord = Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area)
Elevator Area given Hinge Moment Coefficient
Go Elevator Area = Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord)
Elevator Hinge moment coefficient
Go Hinge Moment Coefficient = Hinge Moment/(0.5*Density*Flight Velocity^2*Elevator Area*Elevator Chord)
Elevator Hinge Moment given Hinge Moment Coefficient
Go Hinge Moment = Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Area*Elevator Chord
Stick deflection angle for given stick force
Go Stick Deflection Angle = Hinge Moment*Elevator Deflection Angle/(Stick Force*Stick Length)
Stick length for given stick force
Go Stick Length = Hinge Moment*Elevator Deflection Angle/(Stick Force*Stick Deflection Angle)
Elevator Stick Force
Go Stick Force = Elevator Deflection Angle*Hinge Moment/(Stick Length*Stick Deflection Angle)
Elevator deflection angle for given stick force
Go Elevator Deflection Angle = Stick Force*Stick Length*Stick Deflection Angle/Hinge Moment
Hinge moment for given stick force
Go Hinge Moment = Stick Force*Stick Length*Stick Deflection Angle/Elevator Deflection Angle
Stick deflection angle for given gearing ratio
Go Stick Deflection Angle = Elevator Deflection Angle/(Stick Length*Gearing Ratio)
Control stick length for given gearing ratio
Go Stick Length = Elevator Deflection Angle/(Gearing Ratio*Stick Deflection Angle)
Gearing ratio
Go Gearing Ratio = Elevator Deflection Angle/(Stick Length*Stick Deflection Angle)
Elevator Deflection Angle given Gearing Ratio
Go Elevator Deflection Angle = Gearing Ratio*Stick Length*Stick Deflection Angle
Elevator Stick Force given Gearing Ratio
Go Stick Force = Gearing Ratio*Hinge Moment
Hinge moment for given gearing ratio
Go Hinge Moment = Stick Force/Gearing Ratio
Gearing ratio for given stick force
Go Gearing Ratio = Stick Force/Hinge Moment

Elevator Area given Stick Force Formula

Elevator Area = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord)
Se = ๐™/(๐‘ฎ*Che*0.5*ฯ*V^2*ce)

What is NOTOC?

The NOtification TO Captain (NOTOC) is an essential document for the flight crew. It is the sole source of information to assess the severity of an inflight incident involving dangerous goods carried as cargo.

How to Calculate Elevator Area given Stick Force?

Elevator Area given Stick Force calculator uses Elevator Area = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord) to calculate the Elevator Area, The Elevator area given stick force is a function of the control system's gearing ratio, hinge moment coefficient, elevator chord length, flight altitude, and velocity. Elevator Area is denoted by Se symbol.

How to calculate Elevator Area given Stick Force using this online calculator? To use this online calculator for Elevator Area given Stick Force, enter Stick Force (๐™), Gearing Ratio (๐‘ฎ), Hinge Moment Coefficient (Che), Density (ฯ), Flight Velocity (V) & Elevator Chord (ce) and hit the calculate button. Here is how the Elevator Area given Stick Force calculation can be explained with given input values -> 0.024541 = 23.25/(0.93*0.77*0.5*1.225*60^2*0.6).

FAQ

What is Elevator Area given Stick Force?
The Elevator area given stick force is a function of the control system's gearing ratio, hinge moment coefficient, elevator chord length, flight altitude, and velocity and is represented as Se = ๐™/(๐‘ฎ*Che*0.5*ฯ*V^2*ce) or Elevator Area = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*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, Flight Velocity refers to the speed at which an aircraft moves through the air & Elevator chord is the chord length of an elevator measured from its hinge line to trailing edge.
How to calculate Elevator Area given Stick Force?
The Elevator area given stick force is a function of the control system's gearing ratio, hinge moment coefficient, elevator chord length, flight altitude, and velocity is calculated using Elevator Area = Stick Force/(Gearing Ratio*Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord). To calculate Elevator Area given Stick Force, you need Stick Force (๐™), Gearing Ratio (๐‘ฎ), Hinge Moment Coefficient (Che), Density (ฯ), Flight Velocity (V) & Elevator Chord (ce). With our tool, you need to enter the respective value for Stick Force, Gearing Ratio, Hinge Moment Coefficient, Density, Flight Velocity & 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 Elevator Area?
In this formula, Elevator Area uses Stick Force, Gearing Ratio, Hinge Moment Coefficient, Density, Flight Velocity & Elevator Chord. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Elevator Area = Hinge Moment/(Hinge Moment Coefficient*0.5*Density*Flight Velocity^2*Elevator Chord)
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