Stanton Number Obtained from Classical Theory Formula

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The Stanton Number is a dimensionless quantity that characterizes the heat transfer between a fluid and a solid surface in hypersonic flow conditions. Check FAQs
St=0.332RelPr-23
St - Stanton Number?Rel - Local Reynolds Number?Pr - Prandtl Number?

Stanton Number Obtained from Classical Theory Example

With values
With units
Only example

Here is how the Stanton Number Obtained from Classical Theory equation looks like with Values.

Here is how the Stanton Number Obtained from Classical Theory equation looks like with Units.

Here is how the Stanton Number Obtained from Classical Theory equation looks like.

0.0158Edit=0.332708.3206Edit0.7Edit-23
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Stanton Number Obtained from Classical Theory Solution

Follow our step by step solution on how to calculate Stanton Number Obtained from Classical Theory?

FIRST Step Consider the formula
St=0.332RelPr-23
Next Step Substitute values of Variables
St=0.332708.32060.7-23
Next Step Prepare to Evaluate
St=0.332708.32060.7-23
Next Step Evaluate
St=0.0158230835315729
LAST Step Rounding Answer
St=0.0158

Stanton Number Obtained from Classical Theory Formula Elements

Variables
Functions
Stanton Number
The Stanton Number is a dimensionless quantity that characterizes the heat transfer between a fluid and a solid surface in hypersonic flow conditions.
Symbol: St
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Local Reynolds Number
The Local Reynolds Number is a dimensionless quantity that characterizes the flow regime around a flat plate in viscous flow, indicating whether the flow is laminar or turbulent.
Symbol: Rel
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Prandtl Number
The Prandtl Number is a dimensionless quantity that relates the rate of momentum diffusion to thermal diffusion in fluid flow, indicating the relative importance of these processes.
Symbol: Pr
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
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 in Reference Temperature Method category

​Go Local Reynolds Number
Rel=(1.328Cf)2
​Go Reynolds Number for Chord Length
Rec=ρeueLChordμe
​Go Static Density of Plate using Chord Length for Flat Plate Case
ρe=RecμeueLChord
​Go Static Velocity of Plate using Chord Length for Flat Plate Case
ue=RecμeρeLChord

How to Evaluate Stanton Number Obtained from Classical Theory?

Stanton Number Obtained from Classical Theory evaluator uses Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3) to evaluate the Stanton Number, Stanton Number Obtained from Classical Theory formula is defined as a dimensionless number that characterizes the heat transfer between a fluid and a flat plate, providing a measure of the convective heat transfer coefficient in viscous flow cases. Stanton Number is denoted by St symbol.

How to evaluate Stanton Number Obtained from Classical Theory using this online evaluator? To use this online evaluator for Stanton Number Obtained from Classical Theory, enter Local Reynolds Number (Rel) & Prandtl Number (Pr) and hit the calculate button.

FAQs on Stanton Number Obtained from Classical Theory

What is the formula to find Stanton Number Obtained from Classical Theory?
The formula of Stanton Number Obtained from Classical Theory is expressed as Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3). Here is an example- 0.015823 = 0.332/sqrt(708.3206)*0.7^(-2/3).
How to calculate Stanton Number Obtained from Classical Theory?
With Local Reynolds Number (Rel) & Prandtl Number (Pr) we can find Stanton Number Obtained from Classical Theory using the formula - Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3). This formula also uses Square Root (sqrt) function(s).
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