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Weight of Aircraft in Level, Unaccelerated Flight Formula

GoWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle Formula

GoWeight of Aircraft for given Coefficients of Lift and Drag Formula

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Weight of Body is the force acting on the object due to gravity. Check FAQs

W body = F L + (T \cdot \sin (σ T))

W_body - Weight of Body?F_L - Lift Force?T - Thrust?σ_T - Thrust Angle?

Weight of Aircraft in Level, Unaccelerated Flight Example

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Here is how the Weight of Aircraft in Level, Unaccelerated Flight equation looks like with Values.

Here is how the Weight of Aircraft in Level, Unaccelerated Flight equation looks like with Units.

Here is how the Weight of Aircraft in Level, Unaccelerated Flight equation looks like.

221 = 220 + (100 \cdot \sin (0.01))

221N = 220N + (100N \cdot \sin (0.01rad))

221 = 220 + (100 \cdot \sin (0.01))

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Weight of Aircraft in Level, Unaccelerated Flight Solution

Follow our step by step solution on how to calculate Weight of Aircraft in Level, Unaccelerated Flight?

FIRST Step Consider the formula

W body = F L + (T \cdot \sin (σ T))

Next Step Substitute values of Variables

∴

W body = 220N + (100N \cdot \sin (0.01rad))

Next Step Prepare to Evaluate

∴

W body = 220 + (100 \cdot \sin (0.01))

Next Step Evaluate

∴

W body = 220.999983333417N

LAST Step Rounding Answer

∴

W body = 221N

Weight of Aircraft in Level, Unaccelerated Flight Formula Elements

Variables

Functions

Weight of Body

Weight of Body is the force acting on the object due to gravity.

Symbol: W_body

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Weight of Body

Lift Force

The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.

Symbol: F_L

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Lift Force

Thrust

The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.

Symbol: T

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Thrust

Thrust Angle

Thrust Angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.

Symbol: σ_T

Measurement: AngleUnit: rad

Note: Value can be positive or negative.

Formulas to find Thrust 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 to find Weight of Body

Go Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle

W body = P dynamic \cdot A \cdot C L

Go Weight of Aircraft for given Coefficients of Lift and Drag

W body = C L \cdot \frac{T}{C D}

Go Weight of Aircraft for given Lift-to-Drag Ratio

W body = T \cdot LD

Go Weight of aircraft for given required power

W body = P \cdot \frac{C L}{V ∞ \cdot C D}

Other formulas in Thrust and Power Requirements category

Go Thrust for Level and Unaccelerated Flight

T = \frac{F D}{\cos (σ T)}

Go Thrust Angle for Unaccelerated Level Flight for given Drag

σ T = a \cos (\frac{F D}{T})

Go Thrust Angle for Unaccelerated Level Flight for given Lift

σ T = a \sin (\frac{W body - F L}{T})

Go Thrust of Aircraft required for Level, Unaccelerated Flight

T = P dynamic \cdot A \cdot C D

How to Evaluate Weight of Aircraft in Level, Unaccelerated Flight?

Weight of Aircraft in Level, Unaccelerated Flight evaluator uses Weight of Body = Lift Force+(Thrust*sin(Thrust Angle)) to evaluate the Weight of Body, The Weight of Aircraft in Level, Unaccelerated Flight is the force exerted by gravity on the mass of the aircraft while it maintains a constant velocity and altitude without changing direction, in this state, the sum of all forces acting on the aircraft is balanced, resulting in a net force of zero in any direction, including vertically. Weight of Body is denoted by W_body symbol.

How to evaluate Weight of Aircraft in Level, Unaccelerated Flight using this online evaluator? To use this online evaluator for Weight of Aircraft in Level, Unaccelerated Flight, enter Lift Force (F_L), Thrust (T) & Thrust Angle (σ_T) and hit the calculate button.

FAQs on Weight of Aircraft in Level, Unaccelerated Flight

What is the formula to find Weight of Aircraft in Level, Unaccelerated Flight?

The formula of Weight of Aircraft in Level, Unaccelerated Flight is expressed as Weight of Body = Lift Force+(Thrust*sin(Thrust Angle)). Here is an example- 244.1586 = 220+(100*sin(0.01)).

How to calculate Weight of Aircraft in Level, Unaccelerated Flight?

With Lift Force (F_L), Thrust (T) & Thrust Angle (σ_T) we can find Weight of Aircraft in Level, Unaccelerated Flight using the formula - Weight of Body = Lift Force+(Thrust*sin(Thrust Angle)). This formula also uses Sine (sin) function(s).

What are the other ways to Calculate Weight of Body?

Here are the different ways to Calculate Weight of Body-

Weight of Body=Dynamic Pressure*Area*Lift Coefficient
Weight of Body=Lift Coefficient*Thrust/Drag Coefficient
Weight of Body=Thrust*Lift-to-Drag Ratio

Can the Weight of Aircraft in Level, Unaccelerated Flight be negative?

No, the Weight of Aircraft in Level, Unaccelerated Flight, measured in Force cannot be negative.

Which unit is used to measure Weight of Aircraft in Level, Unaccelerated Flight?

Weight of Aircraft in Level, Unaccelerated Flight is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Weight of Aircraft in Level, Unaccelerated Flight can be measured.

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Weight of Aircraft in Level, Unaccelerated Flight Formula

​GoWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle Formula

​GoWeight of Aircraft for given Coefficients of Lift and Drag Formula

Weight of Aircraft in Level, Unaccelerated Flight Example

Weight of Aircraft in Level, Unaccelerated Flight Solution

Weight of Aircraft in Level, Unaccelerated Flight Formula Elements

Other Formulas to find Weight of Body

Other formulas in Thrust and Power Requirements category

How to Evaluate Weight of Aircraft in Level, Unaccelerated Flight?

FAQs on Weight of Aircraft in Level, Unaccelerated Flight

Variable Name

GoWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle Formula

GoWeight of Aircraft for given Coefficients of Lift and Drag Formula