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Taper Ratio of Airfoil Formula

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Taper Ratio is the ratio of the tip chord to the root chord. Check FAQs

Λ = \frac{C tip}{C root}

Λ - Taper Ratio?C_tip - Tip Chord Length?C_root - Root Chord Length?

Taper Ratio of Airfoil Example

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Here is how the Taper Ratio of Airfoil equation looks like with Values.

Here is how the Taper Ratio of Airfoil equation looks like with Units.

Here is how the Taper Ratio of Airfoil equation looks like.

0.4286 = \frac{3}{7}

0.4286 = \frac{3m}{7m}

0.4286 = \frac{3}{7}

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Taper Ratio of Airfoil Solution

Follow our step by step solution on how to calculate Taper Ratio of Airfoil?

FIRST Step Consider the formula

Λ = \frac{C tip}{C root}

Next Step Substitute values of Variables

∴

Λ = \frac{3m}{7m}

Next Step Prepare to Evaluate

∴

Λ = \frac{3}{7}

Next Step Evaluate

∴

Λ = 0.428571428571429

LAST Step Rounding Answer

∴

Λ = 0.4286

Taper Ratio of Airfoil Formula Elements

Variables

Taper Ratio

Taper Ratio is the ratio of the tip chord to the root chord.

Symbol: Λ

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Taper Ratio

Tip Chord Length

Tip Chord Length, measured parallel to the plane of symmetry, and at points where straight leading or trailing edges meet the curvature at the tip.

Symbol: C_tip

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Tip Chord Length

Root Chord Length

Root Chord Length is the chord length of the root airfoil, which is attached to the fuselage.

Symbol: C_root

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Root Chord Length

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How to Evaluate Taper Ratio of Airfoil?

Taper Ratio of Airfoil evaluator uses Taper Ratio = Tip Chord Length/Root Chord Length to evaluate the Taper Ratio, The Taper Ratio of Airfoil refers to the ratio of the chord length at the wing root (base) to the chord length at the wing tip,it's a geometric parameter that describes how the width of the wing changes from the base to the tip. Taper Ratio is denoted by Λ symbol.

How to evaluate Taper Ratio of Airfoil using this online evaluator? To use this online evaluator for Taper Ratio of Airfoil, enter Tip Chord Length (C_tip) & Root Chord Length (C_root) and hit the calculate button.

FAQs on Taper Ratio of Airfoil

What is the formula to find Taper Ratio of Airfoil?

The formula of Taper Ratio of Airfoil is expressed as Taper Ratio = Tip Chord Length/Root Chord Length. Here is an example- 0.428571 = 3/7.

How to calculate Taper Ratio of Airfoil?

With Tip Chord Length (C_tip) & Root Chord Length (C_root) we can find Taper Ratio of Airfoil using the formula - Taper Ratio = Tip Chord Length/Root Chord Length.

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Taper Ratio of Airfoil Formula

Taper Ratio of Airfoil Example

Taper Ratio of Airfoil Solution

Taper Ratio of Airfoil Formula Elements

Other formulas in Aerodynamic Design category

How to Evaluate Taper Ratio of Airfoil?

FAQs on Taper Ratio of Airfoil

Variable Name