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Datum Length of Aircraft given Deviation of main Undercarriage Formula

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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. Check FAQs

D L = \frac{γ}{\sin (β)}

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

Datum Length of Aircraft given Deviation of main Undercarriage Example

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Here is how the Datum Length of Aircraft given Deviation of main Undercarriage equation looks like with Values.

Here is how the Datum Length of Aircraft given Deviation of main Undercarriage equation looks like with Units.

Here is how the Datum Length of Aircraft given Deviation of main Undercarriage equation looks like.

132.0655 = \frac{95}{\sin (46)}

132.0655m = \frac{95}{\sin (46°)}

132.0655 = \frac{95}{\sin (46)}

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Datum Length of Aircraft given Deviation of main Undercarriage Solution

Follow our step by step solution on how to calculate Datum Length of Aircraft given Deviation of main Undercarriage?

FIRST Step Consider the formula

D L = \frac{γ}{\sin (β)}

Next Step Substitute values of Variables

∴

D L = \frac{95}{\sin (46°)}

Next Step Convert Units

∴

D L = \frac{95}{\sin (0.8029rad)}

Next Step Prepare to Evaluate

∴

D L = \frac{95}{\sin (0.8029)}

Next Step Evaluate

∴

D L = 132.065541146604m

LAST Step Rounding Answer

∴

D L = 132.0655m

Datum Length of Aircraft given Deviation of main Undercarriage Formula Elements

Variables

Functions

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

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.

Symbol: γ

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Deviation of Main Undercarriage

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 Deviation of Main Undercarriage

γ = D L \cdot \sin (β)

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

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

FAQs on Datum Length of Aircraft given Deviation of main Undercarriage

What is the formula to find Datum Length of Aircraft given Deviation of main Undercarriage?

The formula of Datum Length of Aircraft given Deviation of main Undercarriage is expressed as Datum Length of Aircraft = Deviation of Main Undercarriage/sin(Steering Angle). Here is an example- 132.0655 = 95/sin(0.802851455917241).

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

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

Can the Datum Length of Aircraft given Deviation of main Undercarriage be negative?

Yes, the Datum Length of Aircraft given Deviation of main Undercarriage, measured in Length can be negative.

Which unit is used to measure Datum Length of Aircraft given Deviation of main Undercarriage?

Datum Length of Aircraft given Deviation of main Undercarriage is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Datum Length of Aircraft given Deviation of main Undercarriage can be measured.

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Datum Length of Aircraft given Deviation of main Undercarriage Formula

Datum Length of Aircraft given Deviation of main Undercarriage Example

Datum Length of Aircraft given Deviation of main Undercarriage Solution

Datum Length of Aircraft given Deviation of main Undercarriage Formula Elements

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

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

FAQs on Datum Length of Aircraft given Deviation of main Undercarriage

Variable Name