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Coefficient of Drag for Blasius's Solution Formula

GoCoefficient of Drag for Reynold Number Formula

GoAverage Coefficient of Drag for Drag Force Formula

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Coefficient of drag for boundary layer flow is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water. Check FAQs

C D = \frac{1.328}{\sqrt{R e}}

C_D - Coefficient of Drag for Boundary Layer Flow?R_e - Reynolds Number for Boundary Layer Flow?

Coefficient of Drag for Blasius's Solution Example

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Here is how the Coefficient of Drag for Blasius's Solution equation looks like with Values.

Here is how the Coefficient of Drag for Blasius's Solution equation looks like with Units.

Here is how the Coefficient of Drag for Blasius's Solution equation looks like.

0.0034 = \frac{1.328}{\sqrt{150000}}

0.0034 = \frac{1.328}{\sqrt{150000}}

0.0034 = \frac{1.328}{\sqrt{150000}}

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Coefficient of Drag for Blasius's Solution Solution

Follow our step by step solution on how to calculate Coefficient of Drag for Blasius's Solution?

FIRST Step Consider the formula

C D = \frac{1.328}{\sqrt{R e}}

Next Step Substitute values of Variables

∴

C D = \frac{1.328}{\sqrt{150000}}

Next Step Prepare to Evaluate

∴

C D = \frac{1.328}{\sqrt{150000}}

Next Step Evaluate

∴

C D = 0.0034288812558423

LAST Step Rounding Answer

∴

C D = 0.0034

Coefficient of Drag for Blasius's Solution Formula Elements

Variables

Functions

Coefficient of Drag for Boundary Layer Flow

Coefficient of drag for boundary layer flow is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.

Symbol: C_D

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Coefficient of Drag for Boundary Layer Flow

Reynolds Number for Boundary Layer Flow

Reynolds Number for boundary layer 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: R_e

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Reynolds Number for Boundary Layer 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 Coefficient of Drag for Boundary Layer Flow

Go Coefficient of Drag for Reynold Number

C D = \frac{1.46}{\sqrt{R e}}

Go Average Coefficient of Drag for Drag Force

C D = \frac{F D}{\frac{1}{2} \cdot ρ f \cdot A \cdot {V ∞}^{2}}

Other formulas in Boundary Layer Flow category

Go Reynold Number at End of Plate

R e = \frac{ρ f \cdot V ∞ \cdot L}{μ}

Go Length of Plate for Reynold Number

L = \frac{R e \cdot μ}{ρ f \cdot V ∞}

Go Velocity of Fluid for Reynold Number

V ∞ = \frac{R e \cdot μ}{ρ f \cdot L}

Go Thickness of Boundary Layer

𝛿 = \frac{5.48 \cdot x}{\sqrt{R e}}

How to Evaluate Coefficient of Drag for Blasius's Solution?

Coefficient of Drag for Blasius's Solution evaluator uses Coefficient of Drag for Boundary Layer Flow = 1.328/(sqrt(Reynolds Number for Boundary Layer Flow)) to evaluate the Coefficient of Drag for Boundary Layer Flow, The Coefficient of drag for Blasius's solution is known by considering the inverse proportion of Reynolds number in square root. Coefficient of Drag for Boundary Layer Flow is denoted by C_D symbol.

How to evaluate Coefficient of Drag for Blasius's Solution using this online evaluator? To use this online evaluator for Coefficient of Drag for Blasius's Solution, enter Reynolds Number for Boundary Layer Flow (R_e) and hit the calculate button.

FAQs on Coefficient of Drag for Blasius's Solution

What is the formula to find Coefficient of Drag for Blasius's Solution?

The formula of Coefficient of Drag for Blasius's Solution is expressed as Coefficient of Drag for Boundary Layer Flow = 1.328/(sqrt(Reynolds Number for Boundary Layer Flow)). Here is an example- 0.003429 = 1.328/(sqrt(150000)).

How to calculate Coefficient of Drag for Blasius's Solution?

With Reynolds Number for Boundary Layer Flow (R_e) we can find Coefficient of Drag for Blasius's Solution using the formula - Coefficient of Drag for Boundary Layer Flow = 1.328/(sqrt(Reynolds Number for Boundary Layer Flow)). This formula also uses Square Root (sqrt) function(s).

What are the other ways to Calculate Coefficient of Drag for Boundary Layer Flow?

Here are the different ways to Calculate Coefficient of Drag for Boundary Layer Flow-

Coefficient of Drag for Boundary Layer Flow=1.46/sqrt(Reynolds Number for Boundary Layer Flow)
Coefficient of Drag for Boundary Layer Flow=Drag Force on Boundary Layer Flow Plate/(1/2*Fluid Density for Boundary Layer Flow*Area of Surface for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow^2)

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