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Deviation of Main Undercarriage Formula

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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. Check FAQs

γ = D L \cdot \sin (β)

γ - Deviation of Main Undercarriage?D_L - Datum Length of Aircraft?β - Steering Angle?

Deviation of Main Undercarriage Example

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Here is how the Deviation of Main Undercarriage equation looks like with Values.

Here is how the Deviation of Main Undercarriage equation looks like with Units.

Here is how the Deviation of Main Undercarriage equation looks like.

94.9529 = 132 \cdot \sin (46)

94.9529 = 132m \cdot \sin (46°)

94.9529 = 132 \cdot \sin (46)

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Deviation of Main Undercarriage Solution

Follow our step by step solution on how to calculate Deviation of Main Undercarriage?

FIRST Step Consider the formula

γ = D L \cdot \sin (β)

Next Step Substitute values of Variables

∴

γ = 132m \cdot \sin (46°)

Next Step Convert Units

∴

γ = 132m \cdot \sin (0.8029rad)

Next Step Prepare to Evaluate

∴

γ = 132 \cdot \sin (0.8029)

Next Step Evaluate

∴

γ = 94.9528536446881

LAST Step Rounding Answer

∴

γ = 94.9529

Deviation of Main Undercarriage Formula Elements

Variables

Functions

Deviation of Main Undercarriage

Symbol: γ

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Deviation of Main Undercarriage

Datum Length of Aircraft

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.

Symbol: D_L

Measurement: LengthUnit: m

Note: Value can be positive or negative.

Formulas to find Datum Length of Aircraft

Steering Angle

Steering Angle is defined as the angle between the front of the vehicle and the steered wheel direction.

Symbol: β

Measurement: AngleUnit: °

Note: Value can be positive or negative.

Formulas to find Steering Angle

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.

Syntax: sin(Angle)

Other formulas in Path followed by the main Undercarriage of Taxiing Aircraft category

Go Datum Length of Aircraft given Deviation of main Undercarriage

D L = \frac{γ}{\sin (β)}

How to Evaluate Deviation of Main Undercarriage?

Deviation of Main Undercarriage evaluator uses Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle) to evaluate 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 evaluate Deviation of Main Undercarriage using this online evaluator? To use this online evaluator for Deviation of Main Undercarriage, enter Datum Length of Aircraft (D_L) & Steering Angle (β) and hit the calculate button.

FAQs on Deviation of Main Undercarriage

What is the formula to find Deviation of Main Undercarriage?

The formula of Deviation of Main Undercarriage is expressed as Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle). Here is an example- 94.95285 = 132*sin(0.802851455917241).

How to calculate Deviation of Main Undercarriage?

With Datum Length of Aircraft (D_L) & Steering Angle (β) we can find Deviation of Main Undercarriage using the formula - Deviation of Main Undercarriage = Datum Length of Aircraft*sin(Steering Angle). This formula also uses Sine function(s).

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Deviation of Main Undercarriage Formula

Deviation of Main Undercarriage Example

Deviation of Main Undercarriage Solution

Deviation of Main Undercarriage Formula Elements

Other formulas in Path followed by the main Undercarriage of Taxiing Aircraft category

How to Evaluate Deviation of Main Undercarriage?

FAQs on Deviation of Main Undercarriage

Variable Name