Coefficient of Friction using Stanton Equation for Incompressible Flow Calculator

✖The Stanton Number is a dimensionless quantity that characterizes the heat transfer in fluid flow, indicating the relationship between heat transfer and fluid dynamics.ⓘ Stanton Number [St]			+10% -10%
✖The Prandtl Number is a dimensionless quantity that relates the rate of momentum diffusion to thermal diffusion in fluid flow, influencing heat transfer characteristics.ⓘ Prandtl Number [Pr]			+10% -10%

✖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.ⓘ Coefficient of Friction using Stanton Equation for Incompressible Flow [C_f]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Aero Thermal Dynamics Formulas PDF PDF Image

Coefficient of Friction using Stanton Equation for Incompressible Flow Solution

STEP 0: Pre-Calculation Summary

Formula Used

Overall Skin-friction Drag Coefficient = Stanton Number/(0.5*Prandtl Number^(-2/3))
C_f = St/(0.5*Pr^(-2/3))
This formula uses 3 Variables

Variables Used

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.
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.
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

Stanton Number: 0.005956 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_f = St/(0.5*Pr^(-2/3)) --> 0.005956/(0.5*0.7^(-2/3))

Evaluating ... ...

C_f = 0.00939110532629097

STEP 3: Convert Result to Output's Unit

0.00939110532629097 --> No Conversion Required

FINAL ANSWER

0.00939110532629097 ≈ 0.009391 <-- Overall Skin-friction Drag Coefficient

(Calculation completed in 00.004 seconds)

You are here -

Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Viscous Flow Fundamentals » Aero Thermal Dynamics » Coefficient of Friction using Stanton Equation for Incompressible Flow

Credits

Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ 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

Coefficient of Friction using Stanton Equation for Incompressible Flow Formula

LaTeX Go

Overall Skin-friction Drag Coefficient = Stanton Number/(0.5*Prandtl Number^(-2/3))
C_f = St/(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 the fluid.

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

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

How to calculate Coefficient of Friction using Stanton Equation for Incompressible Flow using this online calculator? To use this online calculator for Coefficient of Friction using Stanton Equation for Incompressible Flow, enter Stanton Number (St) & Prandtl Number (Pr) and hit the calculate button. Here is how the Coefficient of Friction using Stanton Equation for Incompressible Flow calculation can be explained with given input values -> 0.009391 = 0.005956/(0.5*0.7^(-2/3)).

FAQ

What is Coefficient of Friction using Stanton Equation for Incompressible Flow?

Coefficient of Friction using Stanton Equation for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force between a fluid and a solid surface in incompressible flow, providing a fundamental parameter in the study of viscous flow and its applications and is represented as C_f = St/(0.5*Pr^(-2/3)) or Overall Skin-friction Drag Coefficient = Stanton Number/(0.5*Prandtl Number^(-2/3)). The Stanton Number is a dimensionless quantity that characterizes the heat transfer in fluid flow, indicating the relationship between heat transfer and fluid dynamics & 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 Coefficient of Friction using Stanton Equation for Incompressible Flow?

Coefficient of Friction using Stanton Equation for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force between a fluid and a solid surface in incompressible flow, providing a fundamental parameter in the study of viscous flow and its applications is calculated using Overall Skin-friction Drag Coefficient = Stanton Number/(0.5*Prandtl Number^(-2/3)). To calculate Coefficient of Friction using Stanton Equation for Incompressible Flow, you need Stanton Number (St) & Prandtl Number (Pr). With our tool, you need to enter the respective value for Stanton Number & Prandtl Number and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

Home

FREE PDFs

🔍 Search