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Coefficient of Lift given Induced Drag Coefficient Formula

GoCoefficient of Lift given Circulation at Origin Formula

GoCoefficient of Lift given Induced Angle of Attack Formula

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The Lift Coefficient ELD 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,ELD = \sqrt{π \cdot AR ELD \cdot C D,i,ELD}

C_L,ELD - Lift Coefficient ELD?AR_ELD - Wing Aspect Ratio ELD?C_D,i,ELD - Induced Drag Coefficient ELD?π - Archimedes' constant?

Coefficient of Lift given Induced Drag Coefficient Example

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Here is how the Coefficient of Lift given Induced Drag Coefficient equation looks like with Values.

Here is how the Coefficient of Lift given Induced Drag Coefficient equation looks like with Units.

Here is how the Coefficient of Lift given Induced Drag Coefficient equation looks like.

1.4979 = \sqrt{3.1416 \cdot 2.48 \cdot 0.288}

1.4979 = \sqrt{3.1416 \cdot 2.48 \cdot 0.288}

1.4979 = \sqrt{3.1416 \cdot 2.48 \cdot 0.288}

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Coefficient of Lift given Induced Drag Coefficient Solution

Follow our step by step solution on how to calculate Coefficient of Lift given Induced Drag Coefficient?

FIRST Step Consider the formula

C L,ELD = \sqrt{π \cdot AR ELD \cdot C D,i,ELD}

Next Step Substitute values of Variables

∴

C L,ELD = \sqrt{π \cdot 2.48 \cdot 0.288}

Next Step Substitute values of Constants

∴

C L,ELD = \sqrt{3.1416 \cdot 2.48 \cdot 0.288}

Next Step Prepare to Evaluate

∴

C L,ELD = \sqrt{3.1416 \cdot 2.48 \cdot 0.288}

Next Step Evaluate

∴

C L,ELD = 1.49794897673451

LAST Step Rounding Answer

∴

C L,ELD = 1.4979

Coefficient of Lift given Induced Drag Coefficient Formula Elements

Variables

Constants

Functions

Lift Coefficient ELD

The Lift Coefficient ELD 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,ELD

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift Coefficient ELD

Wing Aspect Ratio ELD

Wing Aspect Ratio ELD is defined as the ratio of the square of wingspan to the wing area or wingspan over wing chord for a rectangular planform.

Symbol: AR_ELD

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Wing Aspect Ratio ELD

Induced Drag Coefficient ELD

The Induced Drag Coefficient ELD is a dimensionless parameter that describes a relation between the coefficient of the lift and the aspect ratio.

Symbol: C_D,i,ELD

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Induced Drag Coefficient ELD

Archimedes' constant

Archimedes' constant is a mathematical constant that represents the ratio of the circumference of a circle to its diameter.

Symbol: π

Value: 3.14159265358979323846264338327950288

sqrt

A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.

Syntax: sqrt(Number)

Other Formulas to find Lift Coefficient ELD

Go Coefficient of Lift given Circulation at Origin

C L,ELD = π \cdot b \cdot \frac{Γ o}{2 \cdot V ∞ \cdot S 0}

Go Coefficient of Lift given Induced Angle of Attack

C L,ELD = π \cdot α i \cdot AR ELD

Other formulas in Elliptical Lift Distribution category

Go Circulation at given Distance along Wingspan

Γ = Γ o \cdot \sqrt{1 - {(2 \cdot \frac{a}{b})}^{2}}

Go Lift at given Distance along Wingspan

L = ρ ∞ \cdot V ∞ \cdot Γ o \cdot \sqrt{1 - {(2 \cdot \frac{a}{b})}^{2}}

Go Downwash in Elliptical Lift Distribution

w = - \frac{Γ o}{2 \cdot b}

Go Induced Angle of Attack given Aspect Ratio

α i = \frac{C l}{π \cdot AR ELD}

How to Evaluate Coefficient of Lift given Induced Drag Coefficient?

Coefficient of Lift given Induced Drag Coefficient evaluator uses Lift Coefficient ELD = sqrt(pi*Wing Aspect Ratio ELD*Induced Drag Coefficient ELD) to evaluate the Lift Coefficient ELD, The Coefficient of lift given induced drag coefficient formula calculates the coefficient of lift which is an important parameter for the selection of the aerofoil and the aerodynamic efficiency of the wing. Lift Coefficient ELD is denoted by C_L,ELD symbol.

How to evaluate Coefficient of Lift given Induced Drag Coefficient using this online evaluator? To use this online evaluator for Coefficient of Lift given Induced Drag Coefficient, enter Wing Aspect Ratio ELD (AR_ELD) & Induced Drag Coefficient ELD (C_D,i,ELD) and hit the calculate button.

FAQs on Coefficient of Lift given Induced Drag Coefficient

What is the formula to find Coefficient of Lift given Induced Drag Coefficient?

The formula of Coefficient of Lift given Induced Drag Coefficient is expressed as Lift Coefficient ELD = sqrt(pi*Wing Aspect Ratio ELD*Induced Drag Coefficient ELD). Here is an example- 1.497949 = sqrt(pi*2.48*0.288).

How to calculate Coefficient of Lift given Induced Drag Coefficient?

With Wing Aspect Ratio ELD (AR_ELD) & Induced Drag Coefficient ELD (C_D,i,ELD) we can find Coefficient of Lift given Induced Drag Coefficient using the formula - Lift Coefficient ELD = sqrt(pi*Wing Aspect Ratio ELD*Induced Drag Coefficient ELD). This formula also uses Archimedes' constant and Square Root (sqrt) function(s).

What are the other ways to Calculate Lift Coefficient ELD?

Here are the different ways to Calculate Lift Coefficient ELD-

Lift Coefficient ELD=pi*Wingspan*Circulation at Origin/(2*Freestream Velocity*Reference Area Origin)
Lift Coefficient ELD=pi*Induced Angle of Attack*Wing Aspect Ratio ELD

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Coefficient of Lift given Induced Drag Coefficient Formula

​GoCoefficient of Lift given Circulation at Origin Formula

​GoCoefficient of Lift given Induced Angle of Attack Formula

Coefficient of Lift given Induced Drag Coefficient Example

Coefficient of Lift given Induced Drag Coefficient Solution

Coefficient of Lift given Induced Drag Coefficient Formula Elements

Other Formulas to find Lift Coefficient ELD

Other formulas in Elliptical Lift Distribution category

How to Evaluate Coefficient of Lift given Induced Drag Coefficient?

FAQs on Coefficient of Lift given Induced Drag Coefficient

Variable Name

GoCoefficient of Lift given Circulation at Origin Formula

GoCoefficient of Lift given Induced Angle of Attack Formula