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Stanton Number for Incompressible Flow Formula

GoStanton Equation using Overall Skin Friction Coefficient for Incompressible Flow Formula

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The Stanton Number is a dimensionless quantity that characterizes the heat transfer in fluid flow, indicating the relationship between heat transfer and fluid dynamics. Check FAQs

St = 0.332 \cdot \frac{{Pr}^{- \frac{2}{3}}}{\sqrt{Re}}

St - Stanton Number?Pr - Prandtl Number?Re - Reynolds Number?

Stanton Number for Incompressible Flow Example

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Here is how the Stanton Number for Incompressible Flow equation looks like with Values.

Here is how the Stanton Number for Incompressible Flow equation looks like with Units.

Here is how the Stanton Number for Incompressible Flow equation looks like.

0.006 = 0.332 \cdot \frac{{0.7}^{- \frac{2}{3}}}{\sqrt{5000}}

0.006 = 0.332 \cdot \frac{{0.7}^{- \frac{2}{3}}}{\sqrt{5000}}

0.006 = 0.332 \cdot \frac{{0.7}^{- \frac{2}{3}}}{\sqrt{5000}}

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Stanton Number for Incompressible Flow Solution

Follow our step by step solution on how to calculate Stanton Number for Incompressible Flow?

FIRST Step Consider the formula

St = 0.332 \cdot \frac{{Pr}^{- \frac{2}{3}}}{\sqrt{Re}}

Next Step Substitute values of Variables

∴

St = 0.332 \cdot \frac{{0.7}^{- \frac{2}{3}}}{\sqrt{5000}}

Next Step Prepare to Evaluate

∴

St = 0.332 \cdot \frac{{0.7}^{- \frac{2}{3}}}{\sqrt{5000}}

Next Step Evaluate

∴

St = 0.00595553875154443

LAST Step Rounding Answer

∴

St = 0.006

Stanton Number for Incompressible Flow Formula Elements

Variables

Functions

Stanton Number

The Stanton Number is a dimensionless quantity that characterizes the heat transfer in fluid flow, indicating the relationship between heat transfer and fluid dynamics.

Symbol: St

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Stanton Number

Prandtl Number

The Prandtl Number is a dimensionless quantity that relates the rate of momentum diffusion to thermal diffusion in fluid flow, influencing heat transfer characteristics.

Symbol: Pr

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Prandtl Number

Reynolds Number

The Reynolds Number is a dimensionless quantity that helps predict flow patterns in different fluid flow situations, indicating whether the flow is laminar or turbulent.

Symbol: Re

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Reynolds Number

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 Stanton Number

Go Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow

St = C f \cdot 0.5 \cdot {Pr}^{- \frac{2}{3}}

Other formulas in Aero Thermal Dynamics category

Go Non Dimensional Internal Energy Parameter

e' = \frac{U}{C p \cdot T}

Go Non Dimensional Internal Energy Parameter using Wall-to-Freestream Temperature Ratio

e' = \frac{Tw}{T ∞}

Go Wall Temperature Calculation using Internal Energy Change

Tw = e' \cdot T ∞

Go Aerodynamic Heating to Surface

q w = ρ e \cdot u e \cdot St \cdot (h aw - h w)

How to Evaluate Stanton Number for Incompressible Flow?

Stanton Number for Incompressible Flow evaluator uses Stanton Number = 0.332*(Prandtl Number^(-2/3))/sqrt(Reynolds Number) to evaluate the Stanton Number, Stanton Number for Incompressible Flow formula is defined as a dimensionless quantity used to characterize heat transfer in incompressible flows, particularly in boundary layers, and is an important parameter in the study of convective heat transfer in various engineering applications. Stanton Number is denoted by St symbol.

How to evaluate Stanton Number for Incompressible Flow using this online evaluator? To use this online evaluator for Stanton Number for Incompressible Flow, enter Prandtl Number (Pr) & Reynolds Number (Re) and hit the calculate button.

FAQs on Stanton Number for Incompressible Flow

What is the formula to find Stanton Number for Incompressible Flow?

The formula of Stanton Number for Incompressible Flow is expressed as Stanton Number = 0.332*(Prandtl Number^(-2/3))/sqrt(Reynolds Number). Here is an example- 0.005956 = 0.332*(0.7^(-2/3))/sqrt(5000).

How to calculate Stanton Number for Incompressible Flow?

With Prandtl Number (Pr) & Reynolds Number (Re) we can find Stanton Number for Incompressible Flow using the formula - Stanton Number = 0.332*(Prandtl Number^(-2/3))/sqrt(Reynolds Number). This formula also uses Square Root (sqrt) function(s).

What are the other ways to Calculate Stanton Number?

Here are the different ways to Calculate Stanton Number-

Stanton Number=Overall Skin-friction Drag Coefficient*0.5*Prandtl Number^(-2/3)

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Stanton Number for Incompressible Flow Formula

​GoStanton Equation using Overall Skin Friction Coefficient for Incompressible Flow Formula

Stanton Number for Incompressible Flow Example

Stanton Number for Incompressible Flow Solution

Stanton Number for Incompressible Flow Formula Elements

Other Formulas to find Stanton Number

Other formulas in Aero Thermal Dynamics category

How to Evaluate Stanton Number for Incompressible Flow?

FAQs on Stanton Number for Incompressible Flow

Variable Name

GoStanton Equation using Overall Skin Friction Coefficient for Incompressible Flow Formula