Datum Length of Aircraft given Deviation of main Undercarriage Calculator

✖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]			+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%

✖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 given Deviation of main Undercarriage [D_L]

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Datum Length of Aircraft given Deviation of main Undercarriage Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

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.
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.
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

Deviation of Main Undercarriage: 95 --> No Conversion Required
Steering Angle: 46 Degree --> 0.802851455917241 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

D_L = γ/sin(β) --> 95/sin(0.802851455917241)

Evaluating ... ...

D_L = 132.065541146604

STEP 3: Convert Result to Output's Unit

132.065541146604 Meter --> No Conversion Required

FINAL ANSWER

132.065541146604 ≈ 132.0655 Meter <-- Datum Length of Aircraft

(Calculation completed in 00.004 seconds)

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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)

Datum Length of Aircraft given Deviation of main Undercarriage Formula

LaTeX Go

Datum Length of Aircraft = Deviation of Main Undercarriage/sin(Steering Angle)
D_L = γ/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 Datum Length of Aircraft given Deviation of main Undercarriage?

Datum Length of Aircraft given Deviation of main Undercarriage calculator uses Datum Length of Aircraft = Deviation of Main Undercarriage/sin(Steering Angle) to calculate the Datum Length of Aircraft, Datum Length of Aircraft given Deviation of main Undercarriage is defined as length from which conclusions can be inferred. Datum Length of Aircraft is denoted by D_L symbol.

How to calculate Datum Length of Aircraft given Deviation of main Undercarriage using this online calculator? To use this online calculator for Datum Length of Aircraft given Deviation of main Undercarriage, enter Deviation of Main Undercarriage (γ) & Steering Angle (β) and hit the calculate button. Here is how the Datum Length of Aircraft given Deviation of main Undercarriage calculation can be explained with given input values -> 132.0655 = 95/sin(0.802851455917241).

FAQ

What is Datum Length of Aircraft given Deviation of main Undercarriage?

Datum Length of Aircraft given Deviation of main Undercarriage is defined as length from which conclusions can be inferred and is represented as D_L = γ/sin(β) or Datum Length of Aircraft = Deviation of Main Undercarriage/sin(Steering Angle). 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 & Steering Angle is defined as the angle between the front of the vehicle and the steered wheel direction.

How to calculate Datum Length of Aircraft given Deviation of main Undercarriage?

Datum Length of Aircraft given Deviation of main Undercarriage is defined as length from which conclusions can be inferred is calculated using Datum Length of Aircraft = Deviation of Main Undercarriage/sin(Steering Angle). To calculate Datum Length of Aircraft given Deviation of main Undercarriage, you need Deviation of Main Undercarriage (γ) & Steering Angle (β). With our tool, you need to enter the respective value for Deviation of Main Undercarriage & 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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