Stanton Number Obtained from Classical Theory Calculator

✖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.ⓘ Local Reynolds Number [Re_l]			+10% -10%
✖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.ⓘ Prandtl Number [Pr]			+10% -10%

✖The Stanton Number is a dimensionless quantity that characterizes the heat transfer between a fluid and a solid surface in hypersonic flow conditions.ⓘ Stanton Number Obtained from Classical Theory [St]

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Stanton Number Obtained from Classical Theory Solution

STEP 0: Pre-Calculation Summary

Formula Used

Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3)
St = 0.332/sqrt(Re_l)*Pr^(-2/3)
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

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.
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.
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.

STEP 1: Convert Input(s) to Base Unit

Local Reynolds Number: 708.3206 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

St = 0.332/sqrt(Re_l)*Pr^(-2/3) --> 0.332/sqrt(708.3206)*0.7^(-2/3)

Evaluating ... ...

St = 0.0158230835315729

STEP 3: Convert Result to Output's Unit

0.0158230835315729 --> No Conversion Required

FINAL ANSWER

0.0158230835315729 ≈ 0.015823 <-- Stanton Number

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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< Reference Temperature Method Calculators

Static Velocity of Plate using Chord Length for Flat Plate Case

LaTeX Go Static Velocity = (Reynolds Number using Chord Length*Static Viscosity)/(Static Density*Chord Length)

Static Density of Plate using Chord Length for Flat Plate Case

LaTeX Go Static Density = (Reynolds Number using Chord Length*Static Viscosity)/(Static Velocity*Chord Length)

Reynolds Number for Chord Length

LaTeX Go Reynolds Number using Chord Length = Static Density*Static Velocity*Chord Length/Static Viscosity

Local Reynolds Number

LaTeX Go Local Reynolds Number = ((1.328)/Local Skin-Friction Coefficient)^2

Stanton Number Obtained from Classical Theory Formula

LaTeX Go

Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3)
St = 0.332/sqrt(Re_l)*Pr^(-2/3)

What is Heat Transfer Coefficient ?

The heat transfer coefficient or film coefficient, or film effectiveness, in thermodynamics and in mechanics is the proportionality constant between the heat flux and the thermodynamic driving force for the flow of heat.

How to Calculate Stanton Number Obtained from Classical Theory?

Stanton Number Obtained from Classical Theory calculator uses Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3) to calculate 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 calculate Stanton Number Obtained from Classical Theory using this online calculator? To use this online calculator for Stanton Number Obtained from Classical Theory, enter Local Reynolds Number (Re_l) & Prandtl Number (Pr) and hit the calculate button. Here is how the Stanton Number Obtained from Classical Theory calculation can be explained with given input values -> 0.015823 = 0.332/sqrt(708.3206)*0.7^(-2/3).

FAQ

What is Stanton Number Obtained from Classical Theory?

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 and is represented as St = 0.332/sqrt(Re_l)*Pr^(-2/3) or Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3). 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 & 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.

How to calculate Stanton Number Obtained from Classical Theory?

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 is calculated using Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3). To calculate Stanton Number Obtained from Classical Theory, you need Local Reynolds Number (Re_l) & Prandtl Number (Pr). With our tool, you need to enter the respective value for Local Reynolds Number & Prandtl Number and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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