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Induced Drag Coefficient given Aspect Ratio Formula

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

C D,i,ELD = \frac{{C L,ELD}^{2}}{π \cdot AR ELD}

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

Induced Drag Coefficient given Aspect Ratio Example

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Here is how the Induced Drag Coefficient given Aspect Ratio equation looks like with Values.

Here is how the Induced Drag Coefficient given Aspect Ratio equation looks like with Units.

Here is how the Induced Drag Coefficient given Aspect Ratio equation looks like.

0.285 = \frac{{1.49}^{2}}{3.1416 \cdot 2.48}

0.285 = \frac{{1.49}^{2}}{3.1416 \cdot 2.48}

0.285 = \frac{{1.49}^{2}}{3.1416 \cdot 2.48}

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Induced Drag Coefficient given Aspect Ratio Solution

Follow our step by step solution on how to calculate Induced Drag Coefficient given Aspect Ratio?

FIRST Step Consider the formula

C D,i,ELD = \frac{{C L,ELD}^{2}}{π \cdot AR ELD}

Next Step Substitute values of Variables

∴

C D,i,ELD = \frac{{1.49}^{2}}{π \cdot 2.48}

Next Step Substitute values of Constants

∴

C D,i,ELD = \frac{{1.49}^{2}}{3.1416 \cdot 2.48}

Next Step Prepare to Evaluate

∴

C D,i,ELD = \frac{{1.49}^{2}}{3.1416 \cdot 2.48}

Next Step Evaluate

∴

C D,i,ELD = 0.284951523514772

LAST Step Rounding Answer

∴

C D,i,ELD = 0.285

Induced Drag Coefficient given Aspect Ratio Formula Elements

Variables

Constants

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

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

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

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 Induced Drag Coefficient given Aspect Ratio?

Induced Drag Coefficient given Aspect Ratio evaluator uses Induced Drag Coefficient ELD = Lift Coefficient ELD^2/(pi*Wing Aspect Ratio ELD) to evaluate the Induced Drag Coefficient ELD, The Induced drag coefficient given aspect ratio formula calculates the coefficient of induced drag which has been caused due to the element of the air deflected downward which is not vertical to the flight path but is tilted slightly rearward from it. Induced Drag Coefficient ELD is denoted by C_D,i,ELD symbol.

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

FAQs on Induced Drag Coefficient given Aspect Ratio

What is the formula to find Induced Drag Coefficient given Aspect Ratio?

The formula of Induced Drag Coefficient given Aspect Ratio is expressed as Induced Drag Coefficient ELD = Lift Coefficient ELD^2/(pi*Wing Aspect Ratio ELD). Here is an example- 0.288789 = 1.49^2/(pi*2.48).

How to calculate Induced Drag Coefficient given Aspect Ratio?

With Lift Coefficient ELD (C_L,ELD) & Wing Aspect Ratio ELD (AR_ELD) we can find Induced Drag Coefficient given Aspect Ratio using the formula - Induced Drag Coefficient ELD = Lift Coefficient ELD^2/(pi*Wing Aspect Ratio ELD). This formula also uses Archimedes' constant .

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Induced Drag Coefficient given Aspect Ratio Formula

Induced Drag Coefficient given Aspect Ratio Example

Induced Drag Coefficient given Aspect Ratio Solution

Induced Drag Coefficient given Aspect Ratio Formula Elements

Other formulas in Elliptical Lift Distribution category

How to Evaluate Induced Drag Coefficient given Aspect Ratio?

FAQs on Induced Drag Coefficient given Aspect Ratio

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