Deviation of Main Undercarriage Calculator

✖Datum Length of Aircraft observed. A datum is a plane, a straight line, or a point that is used as a reference when processing a material or measuring the dimensions of a target.ⓘ Datum Length of Aircraft [D_L]			+10% -10%
✖Steering Angle is defined as the angle between the front of the vehicle and the steered wheel direction.ⓘ Steering Angle [β]			+10% -10%

✖Deviation of Main Undercarriage observed. The undercarriage of an airplane is the part, including the wheels, which supports the airplane when it is on the ground and when it is landing or taking off.ⓘ Deviation of Main Undercarriage [γ]

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Deviation of Main Undercarriage Solution

STEP 0: Pre-Calculation Summary

Formula Used

Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle)
γ = D_L*sin(β)
This formula uses 1 Functions, 3 Variables

Functions Used

sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)

Variables Used

Deviation of Main Undercarriage - Deviation of Main Undercarriage observed. The undercarriage of an airplane is the part, including the wheels, which supports the airplane when it is on the ground and when it is landing or taking off.
Datum Length of Aircraft - (Measured in Meter) - Datum Length of Aircraft observed. A datum is a plane, a straight line, or a point that is used as a reference when processing a material or measuring the dimensions of a target.
Steering Angle - (Measured in Radian) - Steering Angle is defined as the angle between the front of the vehicle and the steered wheel direction.

STEP 1: Convert Input(s) to Base Unit

Datum Length of Aircraft: 132 Meter --> 132 Meter No Conversion Required
Steering Angle: 46 Degree --> 0.802851455917241 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

γ = D_L*sin(β) --> 132*sin(0.802851455917241)

Evaluating ... ...

γ = 94.9528536446881

STEP 3: Convert Result to Output's Unit

94.9528536446881 --> No Conversion Required

FINAL ANSWER

94.9528536446881 ≈ 94.95285 <-- Deviation of Main Undercarriage

(Calculation completed in 00.004 seconds)

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Created by Mithila Muthamma PA

Coorg Institute of Technology (CIT), Coorg

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< Path followed by the main Undercarriage of Taxiing Aircraft Calculators

Datum Length of Aircraft given Deviation of main Undercarriage

LaTeX Go Datum Length of Aircraft = Deviation of Main Undercarriage/sin(Steering Angle)

Deviation of Main Undercarriage

LaTeX Go Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle)

Deviation of Main Undercarriage Formula

LaTeX Go

Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle)
γ = D_L*sin(β)

What is the function of Taxiway?

The functions of the Taxiway are to: Provide for aircraft to travel to and from runways to other areas of the airport in an expeditious manner. The system of taxiway is a decisive influence on the capacity of the runway system, and thereby also the overall capacity of the aerodrome.

How to Calculate Deviation of Main Undercarriage?

Deviation of Main Undercarriage calculator uses Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle) to calculate the Deviation of Main Undercarriage, The Deviation of Main Undercarriage is defined when the datum point has covered the distance along straight segment of the guideline, for an assumed steering angle. Deviation of Main Undercarriage is denoted by γ symbol.

How to calculate Deviation of Main Undercarriage using this online calculator? To use this online calculator for Deviation of Main Undercarriage, enter Datum Length of Aircraft (D_L) & Steering Angle (β) and hit the calculate button. Here is how the Deviation of Main Undercarriage calculation can be explained with given input values -> 94.95285 = 132*sin(0.802851455917241).

FAQ

What is Deviation of Main Undercarriage?

The Deviation of Main Undercarriage is defined when the datum point has covered the distance along straight segment of the guideline, for an assumed steering angle and is represented as γ = D_L*sin(β) or Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle). Datum Length of Aircraft observed. A datum is a plane, a straight line, or a point that is used as a reference when processing a material or measuring the dimensions of a target & Steering Angle is defined as the angle between the front of the vehicle and the steered wheel direction.

How to calculate Deviation of Main Undercarriage?

The Deviation of Main Undercarriage is defined when the datum point has covered the distance along straight segment of the guideline, for an assumed steering angle is calculated using Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle). To calculate Deviation of Main Undercarriage, you need Datum Length of Aircraft (D_L) & Steering Angle (β). With our tool, you need to enter the respective value for Datum Length of Aircraft & Steering Angle and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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