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Skin Friction Drag Coefficient for Flat Plate in Laminar Flow Formula

GoSkin Friction Drag Coefficient for Flat Plate in Turbulent 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{1.328}{\sqrt{Re L}}

C_f - Skin Friction Drag Coefficient?Re_L - Reynolds Number for Laminar Flow?

Skin Friction Drag Coefficient for Flat Plate in Laminar Flow Example

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

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

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

0.0313 = \frac{1.328}{\sqrt{1800}}

0.0313 = \frac{1.328}{\sqrt{1800}}

0.0313 = \frac{1.328}{\sqrt{1800}}

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Skin Friction Drag Coefficient for Flat Plate in Laminar Flow Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

C f = \frac{1.328}{\sqrt{1800}}

Next Step Prepare to Evaluate

∴

C f = \frac{1.328}{\sqrt{1800}}

Next Step Evaluate

∴

C f = 0.0313012601805245

LAST Step Rounding Answer

∴

C f = 0.0313

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

Variables

Functions

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 Laminar Flow

Reynolds Number for Laminar 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_L

Measurement: NAUnit: Unitless

Note: Value should be between 0 to 2000.

Formulas to find Reynolds Number for Laminar Flow

sqrt

A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.

Syntax: sqrt(Number)

Other Formulas to find Skin Friction Drag Coefficient

Go Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow

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

Other formulas in Flow over Airfoils category

Go Lift Coefficient for Symmetrical Airfoil by Thin Airfoil Theory

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 Laminar Flow?

Skin Friction Drag Coefficient for Flat Plate in Laminar Flow evaluator uses Skin Friction Drag Coefficient = 1.328/(sqrt(Reynolds Number for Laminar Flow)) to evaluate the Skin Friction Drag Coefficient, Skin Friction Drag Coefficient for Flat Plate in Laminar Flow formula can be estimated using the Blasius solution, which provides a relationship between the skin friction coefficient and 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 Laminar Flow using this online evaluator? To use this online evaluator for Skin Friction Drag Coefficient for Flat Plate in Laminar Flow, enter Reynolds Number for Laminar Flow (Re_L) and hit the calculate button.

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

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

The formula of Skin Friction Drag Coefficient for Flat Plate in Laminar Flow is expressed as Skin Friction Drag Coefficient = 1.328/(sqrt(Reynolds Number for Laminar Flow)). Here is an example- 0.031301 = 1.328/(sqrt(1800)).

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

With Reynolds Number for Laminar Flow (Re_L) we can find Skin Friction Drag Coefficient for Flat Plate in Laminar Flow using the formula - Skin Friction Drag Coefficient = 1.328/(sqrt(Reynolds Number for Laminar Flow)). This formula also uses Square Root Function function(s).

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=0.074/(Reynolds Number for Turbulent Flow^(1/5))

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