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

GoWeight of Aircraft in Level, Unaccelerated Flight Formula

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

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

W body = T \cdot LD

W_body - Weight of Body?T - Thrust?LD - Lift-to-Drag Ratio?

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

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Here is how the Weight of Aircraft for given Lift-to-Drag Ratio equation looks like with Values.

Here is how the Weight of Aircraft for given Lift-to-Drag Ratio equation looks like with Units.

Here is how the Weight of Aircraft for given Lift-to-Drag Ratio equation looks like.

221 = 100 \cdot 2.21

221N = 100N \cdot 2.21

221 = 100 \cdot 2.21

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

Follow our step by step solution on how to calculate Weight of Aircraft for given Lift-to-Drag Ratio?

FIRST Step Consider the formula

W body = T \cdot LD

Next Step Substitute values of Variables

∴

W body = 100N \cdot 2.21

Next Step Prepare to Evaluate

∴

W body = 100 \cdot 2.21

LAST Step Evaluate

∴

W body = 221N

Weight of Aircraft for given Lift-to-Drag Ratio Formula Elements

Variables

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

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

Lift-to-Drag Ratio

The Lift-to-Drag ratio is the amount of lift generated by a wing or vehicle, divided by the aerodynamic drag it creates by moving through the air.

Symbol: LD

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift-to-Drag Ratio

Other Formulas to find Weight of Body

Go Weight of Aircraft in Level, Unaccelerated Flight

W body = F L + (T \cdot \sin (σ T))

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 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 for given Lift-to-Drag Ratio?

Weight of Aircraft for given Lift-to-Drag Ratio evaluator uses Weight of Body = Thrust*Lift-to-Drag Ratio to evaluate the Weight of Body, The Weight of Aircraft for given Lift-to-Drag Ratio refers to the force exerted by gravity on the mass of the aircraft, it is the measure of the aircraft's heaviness or the amount of gravitational force pulling it downward, weight is what keeps an aircraft grounded until it generates sufficient lift to overcome it during takeoff, during flight, the aircraft's weight must be balanced by an equal and opposite force, typically provided by the aerodynamic lift generated by the wings. Weight of Body is denoted by W_body symbol.

How to evaluate Weight of Aircraft for given Lift-to-Drag Ratio using this online evaluator? To use this online evaluator for Weight of Aircraft for given Lift-to-Drag Ratio, enter Thrust (T) & Lift-to-Drag Ratio (LD) and hit the calculate button.

FAQs on Weight of Aircraft for given Lift-to-Drag Ratio

What is the formula to find Weight of Aircraft for given Lift-to-Drag Ratio?

The formula of Weight of Aircraft for given Lift-to-Drag Ratio is expressed as Weight of Body = Thrust*Lift-to-Drag Ratio. Here is an example- 20 = 100*2.21.

How to calculate Weight of Aircraft for given Lift-to-Drag Ratio?

With Thrust (T) & Lift-to-Drag Ratio (LD) we can find Weight of Aircraft for given Lift-to-Drag Ratio using the formula - Weight of Body = Thrust*Lift-to-Drag Ratio.

What are the other ways to Calculate Weight of Body?

Here are the different ways to Calculate Weight of Body-

Weight of Body=Lift Force+(Thrust*sin(Thrust Angle))
Weight of Body=Dynamic Pressure*Area*Lift Coefficient
Weight of Body=Lift Coefficient*Thrust/Drag Coefficient

Can the Weight of Aircraft for given Lift-to-Drag Ratio be negative?

No, the Weight of Aircraft for given Lift-to-Drag Ratio, measured in Force cannot be negative.

Which unit is used to measure Weight of Aircraft for given Lift-to-Drag Ratio?

Weight of Aircraft for given Lift-to-Drag Ratio 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 for given Lift-to-Drag Ratio can be measured.

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

​GoWeight of Aircraft in Level, Unaccelerated Flight Formula

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

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

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

Weight of Aircraft for given Lift-to-Drag Ratio Formula Elements

Other Formulas to find Weight of Body

Other formulas in Thrust and Power Requirements category

How to Evaluate Weight of Aircraft for given Lift-to-Drag Ratio?

FAQs on Weight of Aircraft for given Lift-to-Drag Ratio

Variable Name

GoWeight of Aircraft in Level, Unaccelerated Flight Formula

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