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Reynold Number for Drag Force on Plate Formula

GoReynold Number at End of Plate Formula

GoReynold Number for Drag Coefficient in Blasius's Solution Formula

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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. Check FAQs

R e = {(\frac{F D}{0.73 \cdot b \cdot μ \cdot V ∞})}^{2}

R_e - Reynolds Number for Boundary Layer Flow?F_D - Drag Force on Boundary Layer Flow Plate?b - Breadth of Plate for Boundary Layer Flow?μ - Viscosity of Fluid for Boundary Layer Flow?V_∞ - Freestream Velocity for Boundary Layer Flow?

Reynold Number for Drag Force on Plate Example

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Here is how the Reynold Number for Drag Force on Plate equation looks like with Values.

Here is how the Reynold Number for Drag Force on Plate equation looks like with Units.

Here is how the Reynold Number for Drag Force on Plate equation looks like.

137072.6571 = {(\frac{0.03}{0.73 \cdot 0.74 \cdot 0.001 \cdot 0.15})}^{2}

137072.6571 = {(\frac{0.03N}{0.73 \cdot 0.74m \cdot 0.001N*s/m² \cdot 0.15m/s})}^{2}

137072.6571 = {(\frac{0.03}{0.73 \cdot 0.74 \cdot 0.001 \cdot 0.15})}^{2}

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Reynold Number for Drag Force on Plate Solution

Follow our step by step solution on how to calculate Reynold Number for Drag Force on Plate?

FIRST Step Consider the formula

R e = {(\frac{F D}{0.73 \cdot b \cdot μ \cdot V ∞})}^{2}

Next Step Substitute values of Variables

∴

R e = {(\frac{0.03N}{0.73 \cdot 0.74m \cdot 0.001N*s/m² \cdot 0.15m/s})}^{2}

Next Step Convert Units

∴

R e = {(\frac{0.03N}{0.73 \cdot 0.74m \cdot 0.001Pa*s \cdot 0.15m/s})}^{2}

Next Step Prepare to Evaluate

∴

R e = {(\frac{0.03}{0.73 \cdot 0.74 \cdot 0.001 \cdot 0.15})}^{2}

Next Step Evaluate

∴

R e = 137072.657143864

LAST Step Rounding Answer

∴

R e = 137072.6571

Reynold Number for Drag Force on Plate Formula Elements

Variables

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

Drag Force on Boundary Layer Flow Plate

Drag Force on Boundary Layer Flow Plate is the resisting force experienced by an object moving through a fluid.

Symbol: F_D

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Drag Force on Boundary Layer Flow Plate

Breadth of Plate for Boundary Layer Flow

Breadth of plate for boundary layer flow is the measurement or extent of plate from side to side.

Symbol: b

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Breadth of Plate for Boundary Layer Flow

Viscosity of Fluid for Boundary Layer Flow

Viscosity of Fluid for boundary layer flow is a measure of fluid's resistance to deformation at a given rate.

Symbol: μ

Measurement: Dynamic ViscosityUnit: N*s/m²

Note: Value should be greater than 0.

Formulas to find Viscosity of Fluid for Boundary Layer Flow

Freestream Velocity for Boundary Layer Flow

Freestream velocity for boundary layer flow is the velocity of fluid far upstream of a body, that is before the body has a chance to deflect, slow down the fluid.

Symbol: V_∞

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Freestream Velocity for Boundary Layer Flow

Other Formulas to find Reynolds Number for Boundary Layer Flow

Go Reynold Number at End of Plate

R e = \frac{ρ f \cdot V ∞ \cdot L}{μ}

Go Reynold Number for Drag Coefficient in Blasius's Solution

R e = {(\frac{1.328}{C D})}^{2}

Other formulas in Boundary Layer Flow category

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}}

Go Distance from Leading Edge

x = 𝛿 \cdot \frac{\sqrt{R e}}{5.48}

How to Evaluate Reynold Number for Drag Force on Plate?

Reynold Number for Drag Force on Plate evaluator uses Reynolds Number for Boundary Layer Flow = (Drag Force on Boundary Layer Flow Plate/(0.73*Breadth of Plate for Boundary Layer Flow*Viscosity of Fluid for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow))^2 to evaluate the Reynolds Number for Boundary Layer Flow, The Reynold number for drag force on plate formula is known while considering the square root of the drag force on the plate by the viscosity of the fluid, the velocity of the fluid, and the width of the plate. Reynolds Number for Boundary Layer Flow is denoted by R_e symbol.

How to evaluate Reynold Number for Drag Force on Plate using this online evaluator? To use this online evaluator for Reynold Number for Drag Force on Plate, enter Drag Force on Boundary Layer Flow Plate (F_D), Breadth of Plate for Boundary Layer Flow (b), Viscosity of Fluid for Boundary Layer Flow (μ) & Freestream Velocity for Boundary Layer Flow (V_∞) and hit the calculate button.

FAQs on Reynold Number for Drag Force on Plate

What is the formula to find Reynold Number for Drag Force on Plate?

The formula of Reynold Number for Drag Force on Plate is expressed as Reynolds Number for Boundary Layer Flow = (Drag Force on Boundary Layer Flow Plate/(0.73*Breadth of Plate for Boundary Layer Flow*Viscosity of Fluid for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow))^2. Here is an example- 137072.7 = (0.03/(0.73*0.74*0.001*0.15))^2.

How to calculate Reynold Number for Drag Force on Plate?

With Drag Force on Boundary Layer Flow Plate (F_D), Breadth of Plate for Boundary Layer Flow (b), Viscosity of Fluid for Boundary Layer Flow (μ) & Freestream Velocity for Boundary Layer Flow (V_∞) we can find Reynold Number for Drag Force on Plate using the formula - Reynolds Number for Boundary Layer Flow = (Drag Force on Boundary Layer Flow Plate/(0.73*Breadth of Plate for Boundary Layer Flow*Viscosity of Fluid for Boundary Layer Flow*Freestream Velocity for Boundary Layer Flow))^2.

What are the other ways to Calculate Reynolds Number for Boundary Layer Flow?

Here are the different ways to Calculate Reynolds Number for Boundary Layer Flow-

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
Reynolds Number for Boundary Layer Flow=(1.328/Coefficient of Drag for Boundary Layer Flow)^2

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: Value
: Unit

Reynold Number for Drag Force on Plate Formula

​GoReynold Number at End of Plate Formula

​GoReynold Number for Drag Coefficient in Blasius's Solution Formula

Reynold Number for Drag Force on Plate Example

Reynold Number for Drag Force on Plate Solution

Reynold Number for Drag Force on Plate Formula Elements

Other Formulas to find Reynolds Number for Boundary Layer Flow

Other formulas in Boundary Layer Flow category

How to Evaluate Reynold Number for Drag Force on Plate?

FAQs on Reynold Number for Drag Force on Plate

Variable Name

GoReynold Number at End of Plate Formula

GoReynold Number for Drag Coefficient in Blasius's Solution Formula