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(Rel)*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 number that measures the ratio of heat transferred into a fluid to the thermal capacity of the fluid.
Local Reynolds Number - Local Reynolds Number is the ratio of inertial forces to viscous forces.
Prandtl Number - The Prandtl number (Pr) or Prandtl group is a dimensionless number, named after the German physicist Ludwig Prandtl, defined as the ratio of momentum diffusivity to thermal diffusivity.
STEP 1: Convert Input(s) to Base Unit
Local Reynolds Number: 0.55 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
St = 0.332/sqrt(Rel)*Pr^(-2/3) --> 0.332/sqrt(0.55)*0.7^(-2/3)
Evaluating ... ...
St = 0.567838339840002
STEP 3: Convert Result to Output's Unit
0.567838339840002 --> No Conversion Required
FINAL ANSWER
0.567838339840002 0.567838 <-- Stanton Number
(Calculation completed in 00.004 seconds)

Credits

Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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PSG College of Technology (PSGCT), Coimbatore
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15 Reference Temperature Method Calculators

Mach Number at Reference Temperature
Go Mach Number = sqrt((Reference temperature/Static Temperature-(1+0.58*(Wall Temperature/Static Temperature-1)))/0.032)
Wall Temperature using Reference Temperature
Go Wall Temperature = Static Temperature/0.588*(Reference temperature/Static Temperature-(1+0.032*Mach Number^2))+1
Reference Temperature Equation
Go Reference temperature = Static Temperature*(1+0.032*Mach Number^2+0.58*(Wall Temperature/Static Temperature-1))
Static Velocity of Plate using Chord Length for Flat Plate Case
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
Go Static density = (Reynolds number using chord length*Static Viscosity)/(Static Velocity*Chord Length)
Chord Length for Flat Plate Case
Go Chord Length = (Reynolds number using chord length*Static Viscosity)/(Static Velocity*Static density)
Static Viscosity of Plate using Chord Length for Flat Plate Case
Go Static Viscosity = Static density*Static Velocity*Chord Length/Reynolds number using chord length
Reynolds Number for Chord Length
Go Reynolds number using chord length = Static density*Static Velocity*Chord Length/Static Viscosity
Stanton Number Obtained from Classical Theory
Go Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3)
Overall Skin-Friction Drag Coefficient
Go Overall Skin-friction Drag Coefficient = 1.328/sqrt(Reynolds number using chord length)
Overall Skin-Friction Drag Coefficient for Incompressible Flow
Go Overall Skin-friction Drag Coefficient = 0.02667/(Reynolds number using chord length)^0.139
Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient
Go Reynolds number using chord length = (1.328/Overall Skin-friction Drag Coefficient)^2
Local Turbulent Skin-Friction Coefficient for Incompressible Flow
Go Local Skin-Friction Coefficient = 0.02296/(Local Reynolds Number^0.139)
Local Reynolds Number
Go Local Reynolds Number = (0.664^2)/Local Skin-Friction Coefficient^2
Turbulent Flat-Plate Skin-Friction Coefficient
Go Skin friction coefficient = 0.0592/(Local Reynolds Number)^0.2

Stanton Number Obtained from Classical Theory Formula

Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3)
St = 0.332/sqrt(Rel)*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 the interrelation between the constant(0.332), local Reynolds number, and Prandtl number. 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 (Rel) & 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 -> 0.567838 = 0.332/sqrt(0.55)*0.7^(-2/3).

FAQ

What is Stanton Number Obtained from Classical Theory?
Stanton Number obtained from classical theory formula is defined as the interrelation between the constant(0.332), local Reynolds number, and Prandtl number and is represented as St = 0.332/sqrt(Rel)*Pr^(-2/3) or Stanton Number = 0.332/sqrt(Local Reynolds Number)*Prandtl Number^(-2/3). Local Reynolds Number is the ratio of inertial forces to viscous forces & The Prandtl number (Pr) or Prandtl group is a dimensionless number, named after the German physicist Ludwig Prandtl, defined as the ratio of momentum diffusivity to thermal diffusivity.
How to calculate Stanton Number Obtained from Classical Theory?
Stanton Number obtained from classical theory formula is defined as the interrelation between the constant(0.332), local Reynolds number, and Prandtl number 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 (Rel) & 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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