Distance from Leading Edge for Blasius's Solution Calculator

✖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 [𝛿]			+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%

✖Distance leading edge for boundary layer flow is known as the distance of the leading edge from the plate end.ⓘ Distance from Leading Edge for Blasius's Solution [x]

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Distance from Leading Edge for Blasius's Solution Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

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.
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.
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

Thickness of Boundary Layer: 0.014 Meter --> 0.014 Meter No Conversion Required
Reynolds Number for Boundary Layer Flow: 150000 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

x = 𝛿*sqrt(R_e)/4.91 --> 0.014*sqrt(150000)/4.91

Evaluating ... ...

x = 1.10431297040537

STEP 3: Convert Result to Output's Unit

1.10431297040537 Meter --> No Conversion Required

FINAL ANSWER

1.10431297040537 ≈ 1.104313 Meter <-- Distance Leading Edge for Boundary Layer Flow

(Calculation completed in 00.020 seconds)

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Created by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

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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))

Distance from Leading Edge for Blasius's Solution Formula

LaTeX Go

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

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 Distance from Leading Edge for Blasius's Solution?

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

How to calculate Distance from Leading Edge for Blasius's Solution using this online calculator? To use this online calculator for Distance from Leading Edge for Blasius's Solution, enter Thickness of Boundary Layer (𝛿) & Reynolds Number for Boundary Layer Flow (R_e) and hit the calculate button. Here is how the Distance from Leading Edge for Blasius's Solution calculation can be explained with given input values -> 1.104313 = 0.014*sqrt(150000)/4.91.

FAQ

What is Distance from Leading Edge for Blasius's Solution?

The Distance from leading edge for Blasius's solution is known while considering the terms Reynolds number, and the thickness of the boundary layer and is represented as x = 𝛿*sqrt(R_e)/4.91 or Distance Leading Edge for Boundary Layer Flow = Thickness of Boundary Layer*sqrt(Reynolds Number for Boundary Layer Flow)/4.91. 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 & 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 Distance from Leading Edge for Blasius's Solution?

The Distance from leading edge for Blasius's solution is known while considering the terms Reynolds number, and the thickness of the boundary layer is calculated using Distance Leading Edge for Boundary Layer Flow = Thickness of Boundary Layer*sqrt(Reynolds Number for Boundary Layer Flow)/4.91. To calculate Distance from Leading Edge for Blasius's Solution, you need Thickness of Boundary Layer (𝛿) & Reynolds Number for Boundary Layer Flow (R_e). With our tool, you need to enter the respective value for Thickness of Boundary Layer & 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 Distance Leading Edge for Boundary Layer Flow?

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

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

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