Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number Solution

STEP 0: Pre-Calculation Summary
Formula Used
Stanton Number = Nusselt Number/(Reynolds Number*Prandtl Number)
St = Nu/(Re*Pr)
This formula uses 4 Variables
Variables Used
Stanton Number - The Stanton Number is a dimensionless quantity used to characterize heat transfer and frictional drag in the boundary layer of hypersonic flow.
Nusselt Number - The Nusselt Number is a dimensionless quantity that characterizes the convective heat transfer between a surface and a fluid in hypersonic flow conditions.
Reynolds Number - The Reynolds Number is a dimensionless value that predicts the nature of fluid flow, helping to determine the boundary layer characteristics in hypersonic flow conditions.
Prandtl Number - The Prandtl Number is a dimensionless quantity used to characterize the ratio of momentum diffusivity to thermal diffusivity in a fluid.
STEP 1: Convert Input(s) to Base Unit
Nusselt Number: 1400 --> No Conversion Required
Reynolds Number: 5000 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
St = Nu/(Re*Pr) --> 1400/(5000*0.7)
Evaluating ... ...
St = 0.4
STEP 3: Convert Result to Output's Unit
0.4 --> No Conversion Required
FINAL ANSWER
0.4 <-- Stanton Number
(Calculation completed in 00.020 seconds)

Credits

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Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Verified by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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​ LaTeX ​ Go Nusselt Number = Reynolds Number*Stanton Number*Prandtl Number

Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number Formula

​LaTeX ​Go
Stanton Number = Nusselt Number/(Reynolds Number*Prandtl Number)
St = Nu/(Re*Pr)

What is Reynolds number?

The Reynolds number is the ratio of inertial forces to viscous forces within a fluid which is subjected to relative internal movement due to different fluid velocities

How to Calculate Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number?

Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number calculator uses Stanton Number = Nusselt Number/(Reynolds Number*Prandtl Number) to calculate the Stanton Number, Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number formula is defined as a dimensionless number that characterizes the ratio of heat transfer to friction in a fluid flow, providing a crucial parameter in understanding and analyzing heat transfer phenomena in various engineering applications. Stanton Number is denoted by St symbol.

How to calculate Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number using this online calculator? To use this online calculator for Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number, enter Nusselt Number (Nu), Reynolds Number (Re) & Prandtl Number (Pr) and hit the calculate button. Here is how the Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number calculation can be explained with given input values -> 0.001429 = 1400/(5000*0.7).

FAQ

What is Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number?
Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number formula is defined as a dimensionless number that characterizes the ratio of heat transfer to friction in a fluid flow, providing a crucial parameter in understanding and analyzing heat transfer phenomena in various engineering applications and is represented as St = Nu/(Re*Pr) or Stanton Number = Nusselt Number/(Reynolds Number*Prandtl Number). The Nusselt Number is a dimensionless quantity that characterizes the convective heat transfer between a surface and a fluid in hypersonic flow conditions, The Reynolds Number is a dimensionless value that predicts the nature of fluid flow, helping to determine the boundary layer characteristics in hypersonic flow conditions & The Prandtl Number is a dimensionless quantity used to characterize the ratio of momentum diffusivity to thermal diffusivity in a fluid.
How to calculate Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number?
Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number formula is defined as a dimensionless number that characterizes the ratio of heat transfer to friction in a fluid flow, providing a crucial parameter in understanding and analyzing heat transfer phenomena in various engineering applications is calculated using Stanton Number = Nusselt Number/(Reynolds Number*Prandtl Number). To calculate Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number, you need Nusselt Number (Nu), Reynolds Number (Re) & Prandtl Number (Pr). With our tool, you need to enter the respective value for Nusselt Number, 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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