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Coefficient of Lift for given thrust and weight Formula

GoCoefficient of Lift for given Thrust-to-Weight Ratio Formula

GoLift Coefficient given Minimum required Thrust Formula

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The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. Check FAQs

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

C_L - Lift Coefficient?W_body - Weight of Body?C_D - Drag Coefficient?T - Thrust?

Coefficient of Lift for given thrust and weight Example

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Here is how the Coefficient of Lift for given thrust and weight equation looks like with Values.

Here is how the Coefficient of Lift for given thrust and weight equation looks like with Units.

Here is how the Coefficient of Lift for given thrust and weight equation looks like.

1.105 = 221 \cdot \frac{0.5}{100}

1.105 = 221N \cdot \frac{0.5}{100N}

1.105 = 221 \cdot \frac{0.5}{100}

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Coefficient of Lift for given thrust and weight Solution

Follow our step by step solution on how to calculate Coefficient of Lift for given thrust and weight?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

C L = 221N \cdot \frac{0.5}{100N}

Next Step Prepare to Evaluate

∴

C L = 221 \cdot \frac{0.5}{100}

LAST Step Evaluate

∴

C L = 1.105

Coefficient of Lift for given thrust and weight Formula Elements

Variables

Lift Coefficient

The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

Symbol: C_L

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift Coefficient

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

Drag Coefficient

Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.

Symbol: C_D

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Drag Coefficient

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 to find Lift Coefficient

Go Coefficient of Lift for given Thrust-to-Weight Ratio

C L = \frac{C D}{TW}

Go Lift Coefficient given Minimum required Thrust

C L = \sqrt{π \cdot e \cdot AR \cdot ((\frac{T}{P dynamic \cdot A}) - C D,0)}

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 Coefficient of Lift for given thrust and weight?

Coefficient of Lift for given thrust and weight evaluator uses Lift Coefficient = Weight of Body*Drag Coefficient/Thrust to evaluate the Lift Coefficient, The Coefficient of Lift for given thrust and weight quantifies the lift generated by an airfoil (such as a wing) or an aircraft, it's a dimensionless value that depends on various factors including the shape of the airfoil, the angle of attack, weight and drag. Lift Coefficient is denoted by C_L symbol.

How to evaluate Coefficient of Lift for given thrust and weight using this online evaluator? To use this online evaluator for Coefficient of Lift for given thrust and weight, enter Weight of Body (W_body), Drag Coefficient (C_D) & Thrust (T) and hit the calculate button.

FAQs on Coefficient of Lift for given thrust and weight

What is the formula to find Coefficient of Lift for given thrust and weight?

The formula of Coefficient of Lift for given thrust and weight is expressed as Lift Coefficient = Weight of Body*Drag Coefficient/Thrust. Here is an example- 66.3 = 221*0.5/100.

How to calculate Coefficient of Lift for given thrust and weight?

With Weight of Body (W_body), Drag Coefficient (C_D) & Thrust (T) we can find Coefficient of Lift for given thrust and weight using the formula - Lift Coefficient = Weight of Body*Drag Coefficient/Thrust.

What are the other ways to Calculate Lift Coefficient?

Here are the different ways to Calculate Lift Coefficient-

Lift Coefficient=Drag Coefficient/Thrust-to-Weight Ratio
Lift Coefficient=sqrt(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing*((Thrust/(Dynamic Pressure*Area))-Zero Lift Drag Coefficient))

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Coefficient of Lift for given thrust and weight Formula

​GoCoefficient of Lift for given Thrust-to-Weight Ratio Formula

​GoLift Coefficient given Minimum required Thrust Formula

Coefficient of Lift for given thrust and weight Example

Coefficient of Lift for given thrust and weight Solution

Coefficient of Lift for given thrust and weight Formula Elements

Other Formulas to find Lift Coefficient

Other formulas in Lift and Drag Requirements category

How to Evaluate Coefficient of Lift for given thrust and weight?

FAQs on Coefficient of Lift for given thrust and weight

Variable Name

GoCoefficient of Lift for given Thrust-to-Weight Ratio Formula

GoLift Coefficient given Minimum required Thrust Formula