Thickness of Boundary Layer for Blasius's Solution Calculator

✖Distance leading edge for boundary layer flow is known as the distance of the leading edge from the plate end.ⓘ Distance Leading Edge for Boundary Layer Flow [x]			+10% -10%
✖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.ⓘ Reynolds Number for Boundary Layer Flow [R_e]			+10% -10%

✖The Thickness of Boundary Layer is the distance normal to the wall to a point where the flow velocity has essentially reached the 'asymptotic' velocity.ⓘ Thickness of Boundary Layer for Blasius's Solution [𝛿]

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Thickness of Boundary Layer for Blasius's Solution Solution

STEP 0: Pre-Calculation Summary

Formula Used

Thickness of Boundary Layer = (4.91*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow))
𝛿 = (4.91*x)/(sqrt(R_e))
This formula uses 1 Functions, 3 Variables

Functions Used

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., sqrt(Number)

Variables Used

Thickness of Boundary Layer - (Measured in Meter) - The Thickness of Boundary Layer is the distance normal to the wall to a point where the flow velocity has essentially reached the 'asymptotic' velocity.
Distance Leading Edge for Boundary Layer Flow - (Measured in Meter) - Distance leading edge for boundary layer flow is known as the distance of the leading edge from the plate end.
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.

STEP 1: Convert Input(s) to Base Unit

Distance Leading Edge for Boundary Layer Flow: 1.09 Meter --> 1.09 Meter No Conversion Required
Reynolds Number for Boundary Layer Flow: 150000 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

𝛿 = (4.91*x)/(sqrt(R_e)) --> (4.91*1.09)/(sqrt(150000))

Evaluating ... ...

𝛿 = 0.0138185463803783

STEP 3: Convert Result to Output's Unit

0.0138185463803783 Meter --> No Conversion Required

FINAL ANSWER

0.0138185463803783 ≈ 0.013819 Meter <-- Thickness of Boundary Layer

(Calculation completed in 00.020 seconds)

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< Boundary Layer Flow Calculators

Velocity of Fluid for Reynold Number

LaTeX Go Freestream Velocity for Boundary Layer Flow = (Reynolds Number for Boundary Layer Flow*Viscosity of Fluid for Boundary Layer Flow)/(Fluid Density for Boundary Layer Flow*Length of Plate for Boundary Layer Flow)

Length of Plate for Reynold Number

LaTeX Go Length of Plate for Boundary Layer Flow = (Reynolds Number for Boundary Layer Flow*Viscosity of Fluid for Boundary Layer Flow)/(Fluid Density for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow)

Reynold Number at End of Plate

LaTeX Go Reynolds Number for Boundary Layer Flow = (Fluid Density for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow*Length of Plate for Boundary Layer Flow)/Viscosity of Fluid for Boundary Layer Flow

Thickness of Boundary Layer

LaTeX Go Thickness of Boundary Layer = (5.48*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow))

Thickness of Boundary Layer for Blasius's Solution Formula

LaTeX Go

Thickness of Boundary Layer = (4.91*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow))
𝛿 = (4.91*x)/(sqrt(R_e))

What is Reynolds number in boundary layer flow?

The Reynolds number is the ratio of inertial forces to viscous forces within a fluid that is subjected to relative internal movement due to different fluid velocities. A region where these forces change behavior is known as a boundary layer, such as the bounding surface in the interior of a pipe.

What are the two types of flow associated with the boundary layer?

There are two different types of boundary layer flow: laminar and turbulent. The laminar boundary is a very smooth flow, while the turbulent boundary layer contains swirls or "eddies." The laminar flow creates less skin friction drag than the turbulent flow but is less stable.

How to Calculate Thickness of Boundary Layer for Blasius's Solution?

Thickness of Boundary Layer for Blasius's Solution calculator uses Thickness of Boundary Layer = (4.91*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow)) to calculate the Thickness of Boundary Layer, The Thickness of boundary layer for Blasius's solution formula is known while considering the distance from the leading edge to the square root of the Reynolds number. Thickness of Boundary Layer is denoted by 𝛿 symbol.

How to calculate Thickness of Boundary Layer for Blasius's Solution using this online calculator? To use this online calculator for Thickness of Boundary Layer for Blasius's Solution, enter Distance Leading Edge for Boundary Layer Flow (x) & Reynolds Number for Boundary Layer Flow (R_e) and hit the calculate button. Here is how the Thickness of Boundary Layer for Blasius's Solution calculation can be explained with given input values -> 0.013819 = (4.91*1.09)/(sqrt(150000)).

FAQ

What is Thickness of Boundary Layer for Blasius's Solution?

The Thickness of boundary layer for Blasius's solution formula is known while considering the distance from the leading edge to the square root of the Reynolds number and is represented as 𝛿 = (4.91*x)/(sqrt(R_e)) or Thickness of Boundary Layer = (4.91*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow)). Distance leading edge for boundary layer flow is known as the distance of the leading edge from the plate end & 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.

How to calculate Thickness of Boundary Layer for Blasius's Solution?

The Thickness of boundary layer for Blasius's solution formula is known while considering the distance from the leading edge to the square root of the Reynolds number is calculated using Thickness of Boundary Layer = (4.91*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow)). To calculate Thickness of Boundary Layer for Blasius's Solution, you need Distance Leading Edge for Boundary Layer Flow (x) & Reynolds Number for Boundary Layer Flow (R_e). With our tool, you need to enter the respective value for Distance Leading Edge for Boundary Layer Flow & Reynolds Number for Boundary Layer Flow and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Thickness of Boundary Layer?

In this formula, Thickness of Boundary Layer uses Distance Leading Edge for Boundary Layer Flow & Reynolds Number for Boundary Layer Flow. We can use 1 other way(s) to calculate the same, which is/are as follows -

Thickness of Boundary Layer = (5.48*Distance Leading Edge for Boundary Layer Flow)/(sqrt(Reynolds Number for Boundary Layer Flow))

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