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Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow Formula

GoSkin Friction Drag Coefficient for Flat Plate in Laminar Flow Formula

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Skin Friction Drag Coefficient is obtained by dividing the skin friction drag by the product of dynamic pressure and reference area. Check FAQs

C f = \frac{0.074}{{Re T}^{\frac{1}{5}}}

C_f - Skin Friction Drag Coefficient?Re_T - Reynolds Number for Turbulent Flow?

Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow Example

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Here is how the Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow equation looks like with Values.

Here is how the Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow equation looks like with Units.

Here is how the Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow equation looks like.

0.0145 = \frac{0.074}{3500^{\frac{1}{5}}}

0.0145 = \frac{0.074}{3500^{\frac{1}{5}}}

0.0145 = \frac{0.074}{3500^{\frac{1}{5}}}

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Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow Solution

Follow our step by step solution on how to calculate Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow?

FIRST Step Consider the formula

C f = \frac{0.074}{{Re T}^{\frac{1}{5}}}

Next Step Substitute values of Variables

∴

C f = \frac{0.074}{3500^{\frac{1}{5}}}

Next Step Prepare to Evaluate

∴

C f = \frac{0.074}{3500^{\frac{1}{5}}}

Next Step Evaluate

∴

C f = 0.0144683201748677

LAST Step Rounding Answer

∴

C f = 0.0145

Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow Formula Elements

Variables

Skin Friction Drag Coefficient

Skin Friction Drag Coefficient is obtained by dividing the skin friction drag by the product of dynamic pressure and reference area.

Symbol: C_f

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Skin Friction Drag Coefficient

Reynolds Number for Turbulent Flow

Reynolds Number for Turbulent Flow is the ratio of inertial forces to viscous forces within a fluid which is subjected to relative internal movement due to different fluid velocities.

Symbol: Re_T

Measurement: NAUnit: Unitless

Note: Value should be greater than 2000.

Formulas to find Reynolds Number for Turbulent Flow

Other Formulas to find Skin Friction Drag Coefficient

Go Skin Friction Drag Coefficient for Flat Plate in Laminar Flow

C f = \frac{1.328}{\sqrt{Re L}}

Other formulas in Flow over Airfoils category

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C L = 2 \cdot π \cdot α

Go Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory

C m,le = - \frac{C L}{4}

Go Lift Coefficient for Cambered Airfoil

C L,cam = 2 \cdot π \cdot ((α) - (α 0))

Go Center of Pressure Location for Cambered Airfoil

x cp = - \frac{C m,le \cdot c}{C L}

How to Evaluate Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow?

Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow evaluator uses Skin Friction Drag Coefficient = 0.074/(Reynolds Number for Turbulent Flow^(1/5)) to evaluate the Skin Friction Drag Coefficient, Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow formula can be estimated using the Darcy-Weisbach equation, which relates the skin friction coefficient to the Reynolds number based on distance along the plate. Skin Friction Drag Coefficient is denoted by C_f symbol.

How to evaluate Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow using this online evaluator? To use this online evaluator for Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow, enter Reynolds Number for Turbulent Flow (Re_T) and hit the calculate button.

FAQs on Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow

What is the formula to find Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow?

The formula of Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow is expressed as Skin Friction Drag Coefficient = 0.074/(Reynolds Number for Turbulent Flow^(1/5)). Here is an example- 0.014468 = 0.074/(3500^(1/5)).

How to calculate Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow?

With Reynolds Number for Turbulent Flow (Re_T) we can find Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow using the formula - Skin Friction Drag Coefficient = 0.074/(Reynolds Number for Turbulent Flow^(1/5)).

What are the other ways to Calculate Skin Friction Drag Coefficient?

Here are the different ways to Calculate Skin Friction Drag Coefficient-

Skin Friction Drag Coefficient=1.328/(sqrt(Reynolds Number for Laminar Flow))

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