Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow Solution

STEP 0: Pre-Calculation Summary
Formula Used
Stanton Number = Overall Skin-friction Drag Coefficient*0.5*Prandtl Number^(-2/3)
St = Cf*0.5*Pr^(-2/3)
This formula uses 3 Variables
Variables Used
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.
Overall Skin-friction Drag Coefficient - The Overall Skin-friction Drag Coefficient is a dimensionless number representing the resistance experienced by an object moving through a fluid due to viscous effects.
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.
STEP 1: Convert Input(s) to Base Unit
Overall Skin-friction Drag Coefficient: 0.009391 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
St = Cf*0.5*Pr^(-2/3) --> 0.009391*0.5*0.7^(-2/3)
Evaluating ... ...
St = 0.00595593320026055
STEP 3: Convert Result to Output's Unit
0.00595593320026055 --> No Conversion Required
FINAL ANSWER
0.00595593320026055 0.005956 <-- Stanton Number
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
Shikha Maurya has verified this Calculator and 200+ more calculators!

Aero Thermal Dynamics Calculators

Aerodynamic Heating to Surface
​ LaTeX ​ Go Local Heat Transfer Rate = Static Density*Static Velocity*Stanton Number*(Adiabatic Wall Enthalpy-Wall Enthalpy)
Non Dimensional Internal Energy Parameter
​ LaTeX ​ Go Non-Dimensional Internal Energy = Internal Energy/(Specific Heat Capacity at Constant Pressure*Temperature)
Non Dimensional Internal Energy Parameter using Wall-to-Freestream Temperature Ratio
​ LaTeX ​ Go Non-Dimensional Internal Energy = Wall Temperature/Free Stream Temperature
Wall Temperature Calculation using Internal Energy Change
​ LaTeX ​ Go Wall Temperature = Non-Dimensional Internal Energy*Free Stream Temperature

Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow Formula

​LaTeX ​Go
Stanton Number = Overall Skin-friction Drag Coefficient*0.5*Prandtl Number^(-2/3)
St = Cf*0.5*Pr^(-2/3)

What is Stanton number?

The Stanton number, St, is a dimensionless number that measures the ratio of heat transferred into a fluid to the thermal capacity of fluid

How to Calculate Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow?

Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow calculator uses Stanton Number = Overall Skin-friction Drag Coefficient*0.5*Prandtl Number^(-2/3) to calculate the Stanton Number, Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force exerted by a fluid on a surface, providing a fundamental parameter in the study of viscous flow and heat transfer in incompressible fluids. Stanton Number is denoted by St symbol.

How to calculate Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow using this online calculator? To use this online calculator for Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow, enter Overall Skin-friction Drag Coefficient (Cf) & Prandtl Number (Pr) and hit the calculate button. Here is how the Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow calculation can be explained with given input values -> 1.199939 = 0.009391*0.5*0.7^(-2/3).

FAQ

What is Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow?
Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force exerted by a fluid on a surface, providing a fundamental parameter in the study of viscous flow and heat transfer in incompressible fluids and is represented as St = Cf*0.5*Pr^(-2/3) or Stanton Number = Overall Skin-friction Drag Coefficient*0.5*Prandtl Number^(-2/3). The Overall Skin-friction Drag Coefficient is a dimensionless number representing the resistance experienced by an object moving through a fluid due to viscous effects & The Prandtl Number is a dimensionless quantity that relates the rate of momentum diffusion to thermal diffusion in fluid flow, influencing heat transfer characteristics.
How to calculate Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow?
Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force exerted by a fluid on a surface, providing a fundamental parameter in the study of viscous flow and heat transfer in incompressible fluids is calculated using Stanton Number = Overall Skin-friction Drag Coefficient*0.5*Prandtl Number^(-2/3). To calculate Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow, you need Overall Skin-friction Drag Coefficient (Cf) & Prandtl Number (Pr). With our tool, you need to enter the respective value for Overall Skin-friction Drag Coefficient & Prandtl Number and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Stanton Number?
In this formula, Stanton Number uses Overall Skin-friction Drag Coefficient & Prandtl Number. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Stanton Number = 0.332*(Prandtl Number^(-2/3))/sqrt(Reynolds Number)
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!