FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Aspect Ratio given Induced Drag Coefficient Formula

GoAspect Ratio given Induced Angle of Attack Formula

Fx Copy

LaTeX Copy

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. Check FAQs

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

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

Aspect Ratio given Induced Drag Coefficient Example

With values

With units

Only example

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

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

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

2.4537 = \frac{{1.49}^{2}}{3.1416 \cdot 0.288}

2.4537 = \frac{{1.49}^{2}}{3.1416 \cdot 0.288}

2.4537 = \frac{{1.49}^{2}}{3.1416 \cdot 0.288}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Aerodynamics » fx Aspect Ratio given Induced Drag Coefficient

Aspect Ratio given Induced Drag Coefficient Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

AR ELD = \frac{{1.49}^{2}}{π \cdot 0.288}

Next Step Substitute values of Constants

∴

AR ELD = \frac{{1.49}^{2}}{3.1416 \cdot 0.288}

Next Step Prepare to Evaluate

∴

AR ELD = \frac{{1.49}^{2}}{3.1416 \cdot 0.288}

Next Step Evaluate

∴

AR ELD = 2.45374923026609

LAST Step Rounding Answer

∴

AR ELD = 2.4537

Aspect Ratio given Induced Drag Coefficient Formula Elements

Variables

Constants

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

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

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

Other Formulas to find Wing Aspect Ratio ELD

Go Aspect Ratio given Induced Angle of Attack

AR ELD = \frac{C L,ELD}{π \cdot α i}

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 Aspect Ratio given Induced Drag Coefficient?

Aspect Ratio given Induced Drag Coefficient evaluator uses Wing Aspect Ratio ELD = Lift Coefficient ELD^2/(pi*Induced Drag Coefficient ELD) to evaluate the Wing Aspect Ratio ELD, The Aspect ratio given induced drag coefficient formula calculates the aspect ratio of the wing by using the induced drag coefficient and the coefficient of lift. Wing Aspect Ratio ELD is denoted by AR_ELD symbol.

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

FAQs on Aspect Ratio given Induced Drag Coefficient

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

The formula of Aspect Ratio given Induced Drag Coefficient is expressed as Wing Aspect Ratio ELD = Lift Coefficient ELD^2/(pi*Induced Drag Coefficient ELD). Here is an example- 2.486796 = 1.49^2/(pi*0.288).

How to calculate Aspect Ratio given Induced Drag Coefficient?

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

What are the other ways to Calculate Wing Aspect Ratio ELD?

Here are the different ways to Calculate Wing Aspect Ratio ELD-

Wing Aspect Ratio ELD=Lift Coefficient ELD/(pi*Induced Angle of Attack)

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Aspect Ratio given Induced Drag Coefficient Formula

​GoAspect Ratio given Induced Angle of Attack Formula

Aspect Ratio given Induced Drag Coefficient Example

Aspect Ratio given Induced Drag Coefficient Solution

Aspect Ratio given Induced Drag Coefficient Formula Elements

Other Formulas to find Wing Aspect Ratio ELD

Other formulas in Elliptical Lift Distribution category

How to Evaluate Aspect Ratio given Induced Drag Coefficient?

FAQs on Aspect Ratio given Induced Drag Coefficient

Variable Name

GoAspect Ratio given Induced Angle of Attack Formula