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Lift-to-Drag Ratio given required Thrust of Aircraft Formula

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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. Check FAQs

LD = \frac{W body}{T}

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

Lift-to-Drag Ratio given required Thrust of Aircraft Example

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

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

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

2.21 = \frac{221}{100}

2.21 = \frac{221N}{100N}

2.21 = \frac{221}{100}

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Lift-to-Drag Ratio given required Thrust of Aircraft Solution

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

FIRST Step Consider the formula

LD = \frac{W body}{T}

Next Step Substitute values of Variables

∴

LD = \frac{221N}{100N}

Next Step Prepare to Evaluate

∴

LD = \frac{221}{100}

LAST Step Evaluate

∴

LD = 2.21

Lift-to-Drag Ratio given required Thrust of Aircraft Formula Elements

Variables

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

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

Other formulas in Lift and Drag Requirements category

Go Drag for Level and Unaccelerated Flight

F D = T \cdot \cos (σ T)

Go Lift for Unaccelerated Flight

F L = W body - T \cdot \sin (σ T)

Go Drag for Level and Unaccelerated Flight at Negligible Thrust Angle

F D = P dynamic \cdot A \cdot C D

Go Lift for Level and Unaccelerated Flight at Negligible Thrust Angle

F L = P dynamic \cdot A \cdot C L

How to Evaluate Lift-to-Drag Ratio given required Thrust of Aircraft?

Lift-to-Drag Ratio given required Thrust of Aircraft evaluator uses Lift-to-Drag Ratio = Weight of Body/Thrust to evaluate the Lift-to-Drag Ratio, The Lift-to-Drag Ratio given required Thrust of Aircraft is a measure used in aerodynamics to assess the efficiency of an aircraft's wing design, it is defined as the ratio of the lift generated by the wings to the drag produced by the aircraft as it moves through the air. Lift-to-Drag Ratio is denoted by LD symbol.

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

FAQs on Lift-to-Drag Ratio given required Thrust of Aircraft

What is the formula to find Lift-to-Drag Ratio given required Thrust of Aircraft?

The formula of Lift-to-Drag Ratio given required Thrust of Aircraft is expressed as Lift-to-Drag Ratio = Weight of Body/Thrust. Here is an example- 2.21 = 221/100.

How to calculate Lift-to-Drag Ratio given required Thrust of Aircraft?

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

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Lift-to-Drag Ratio given required Thrust of Aircraft Formula

Lift-to-Drag Ratio given required Thrust of Aircraft Example

Lift-to-Drag Ratio given required Thrust of Aircraft Solution

Lift-to-Drag Ratio given required Thrust of Aircraft Formula Elements

Other formulas in Lift and Drag Requirements category

How to Evaluate Lift-to-Drag Ratio given required Thrust of Aircraft?

FAQs on Lift-to-Drag Ratio given required Thrust of Aircraft

Variable Name