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Induced Drag Factor given Induced Drag Coefficient Formula

GoInduced Drag Factor given Span Efficiency Factor Formula

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The Induced Drag Factor is a function of the Fourier series constants which has been used for the general circulation distribution expression for the finite wing. Check FAQs

δ = \frac{π \cdot AR GLD \cdot C D,i,GLD}{{C L,GLD}^{2}} - 1

δ - Induced Drag Factor?AR_GLD - Wing Aspect Ratio GLD?C_D,i,GLD - Induced Drag Coefficient GLD?C_L,GLD - Lift Coefficient GLD?π - Archimedes' constant?

Induced Drag Factor given Induced Drag Coefficient Example

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

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

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

0.0468 = \frac{3.1416 \cdot 15 \cdot 0.048}{{1.47}^{2}} - 1

0.0468 = \frac{3.1416 \cdot 15 \cdot 0.048}{{1.47}^{2}} - 1

0.0468 = \frac{3.1416 \cdot 15 \cdot 0.048}{{1.47}^{2}} - 1

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Induced Drag Factor given Induced Drag Coefficient Solution

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

FIRST Step Consider the formula

δ = \frac{π \cdot AR GLD \cdot C D,i,GLD}{{C L,GLD}^{2}} - 1

Next Step Substitute values of Variables

∴

δ = \frac{π \cdot 15 \cdot 0.048}{{1.47}^{2}} - 1

Next Step Substitute values of Constants

∴

δ = \frac{3.1416 \cdot 15 \cdot 0.048}{{1.47}^{2}} - 1

Next Step Prepare to Evaluate

∴

δ = \frac{3.1416 \cdot 15 \cdot 0.048}{{1.47}^{2}} - 1

Next Step Evaluate

∴

δ = 0.046761400613009

LAST Step Rounding Answer

∴

δ = 0.0468

Induced Drag Factor given Induced Drag Coefficient Formula Elements

Variables

Constants

Induced Drag Factor

The Induced Drag Factor is a function of the Fourier series constants which has been used for the general circulation distribution expression for the finite wing.

Symbol: δ

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Induced Drag Factor

Wing Aspect Ratio GLD

Wing Aspect Ratio GLD 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_GLD

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Wing Aspect Ratio GLD

Induced Drag Coefficient GLD

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

Symbol: C_D,i,GLD

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Induced Drag Coefficient GLD

Lift Coefficient GLD

The Lift Coefficient GLD 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,GLD

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift Coefficient GLD

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 to find Induced Drag Factor

Go Induced Drag Factor given Span Efficiency Factor

δ = {e span}^{- 1} - 1

Other formulas in General Lift Distribution category

Go Span Efficiency Factor

e span = {(1 + δ)}^{- 1}

Go Lift Coefficient given Span Efficiency Factor

C L,GLD = \sqrt{π \cdot e span \cdot AR GLD \cdot C D,i,GLD}

Go Induced Drag Coefficient given Span Efficiency Factor

C D,i,GLD = \frac{{C L,GLD}^{2}}{π \cdot e span \cdot AR GLD}

Go Induced Lift Slope Factor given Lift Curve Slope of Finite Wing

τ FW = \frac{π \cdot AR GLD \cdot (\frac{a 0}{a C,l} - 1)}{a 0} - 1

How to Evaluate Induced Drag Factor given Induced Drag Coefficient?

Induced Drag Factor given Induced Drag Coefficient evaluator uses Induced Drag Factor = (pi*Wing Aspect Ratio GLD*Induced Drag Coefficient GLD)/Lift Coefficient GLD^2-1 to evaluate the Induced Drag Factor, The Induced drag factor given induced drag coefficient formula calculates induced drag factor which is a function of the Fourier series constants which has been used for the general circulation distribution expression for the finite wing. Induced Drag Factor is denoted by δ symbol.

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

FAQs on Induced Drag Factor given Induced Drag Coefficient

What is the formula to find Induced Drag Factor given Induced Drag Coefficient?

The formula of Induced Drag Factor given Induced Drag Coefficient is expressed as Induced Drag Factor = (pi*Wing Aspect Ratio GLD*Induced Drag Coefficient GLD)/Lift Coefficient GLD^2-1. Here is an example- -0.127699 = (pi*15*0.048)/1.47^2-1.

How to calculate Induced Drag Factor given Induced Drag Coefficient?

With Wing Aspect Ratio GLD (AR_GLD), Induced Drag Coefficient GLD (C_D,i,GLD) & Lift Coefficient GLD (C_L,GLD) we can find Induced Drag Factor given Induced Drag Coefficient using the formula - Induced Drag Factor = (pi*Wing Aspect Ratio GLD*Induced Drag Coefficient GLD)/Lift Coefficient GLD^2-1. This formula also uses Archimedes' constant .

What are the other ways to Calculate Induced Drag Factor?

Here are the different ways to Calculate Induced Drag Factor-

Induced Drag Factor=Span Efficiency Factor^(-1)-1

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: Unit

Induced Drag Factor given Induced Drag Coefficient Formula

​GoInduced Drag Factor given Span Efficiency Factor Formula

Induced Drag Factor given Induced Drag Coefficient Example

Induced Drag Factor given Induced Drag Coefficient Solution

Induced Drag Factor given Induced Drag Coefficient Formula Elements

Other Formulas to find Induced Drag Factor

Other formulas in General Lift Distribution category

How to Evaluate Induced Drag Factor given Induced Drag Coefficient?

FAQs on Induced Drag Factor given Induced Drag Coefficient

Variable Name

GoInduced Drag Factor given Span Efficiency Factor Formula