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

✖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.ⓘ Reynolds Number [Re]			+10% -10%
✖The Stanton Number is a dimensionless quantity used to characterize heat transfer and frictional drag in the boundary layer of hypersonic flow.ⓘ Stanton Number [St]			+10% -10%
✖The Prandtl Number is a dimensionless quantity used to characterize the ratio of momentum diffusivity to thermal diffusivity in a fluid.ⓘ Prandtl Number [Pr]			+10% -10%

✖The Nusselt Number is a dimensionless quantity that characterizes the convective heat transfer between a surface and a fluid in hypersonic flow conditions.ⓘ Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number [N_u]

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

STEP 0: Pre-Calculation Summary

Formula Used

Nusselt Number = Reynolds Number*Stanton Number*Prandtl Number
N_u = Re*St*Pr
This formula uses 4 Variables

Variables Used

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.
Stanton Number - The Stanton Number is a dimensionless quantity used to characterize heat transfer and frictional drag in the boundary layer of hypersonic flow.
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

Reynolds Number: 5000 --> No Conversion Required
Stanton Number: 0.4 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

N_u = Re*St*Pr --> 5000*0.4*0.7

Evaluating ... ...

N_u = 1400

STEP 3: Convert Result to Output's Unit

1400 --> No Conversion Required

FINAL ANSWER

1400 <-- Nusselt 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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< Dimensionless Quantities Calculators

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

LaTeX Go Stanton Number = Nusselt Number/(Reynolds Number*Prandtl Number)

Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number

LaTeX Go Reynolds Number = Nusselt Number/(Stanton Number*Prandtl Number)

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

LaTeX Go Prandtl Number = Nusselt Number/(Stanton Number*Reynolds Number)

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

LaTeX Go Nusselt Number = Reynolds Number*Stanton Number*Prandtl Number

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

LaTeX Go

Nusselt Number = Reynolds Number*Stanton Number*Prandtl Number
N_u = Re*St*Pr

What is Reynolds number ?

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

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

Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number calculator uses Nusselt Number = Reynolds Number*Stanton Number*Prandtl Number to calculate the Nusselt Number, Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number formula is defined as a dimensionless value that characterizes the convective heat transfer between a fluid and a solid surface, commonly used in the context of boundary layer equations for hypersonic flow to analyze heat transfer and fluid flow. Nusselt Number is denoted by N_u symbol.

How to calculate Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number using this online calculator? To use this online calculator for Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number, enter Reynolds Number (Re), Stanton Number (St) & Prandtl Number (Pr) and hit the calculate button. Here is how the Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number calculation can be explained with given input values -> 1400 = 5000*0.4*0.7.

FAQ

What is Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number?

Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number formula is defined as a dimensionless value that characterizes the convective heat transfer between a fluid and a solid surface, commonly used in the context of boundary layer equations for hypersonic flow to analyze heat transfer and fluid flow and is represented as N_u = Re*St*Pr or Nusselt Number = Reynolds Number*Stanton Number*Prandtl 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, The Stanton Number is a dimensionless quantity used to characterize heat transfer and frictional drag in the boundary layer of hypersonic flow & The Prandtl Number is a dimensionless quantity used to characterize the ratio of momentum diffusivity to thermal diffusivity in a fluid.

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

Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number formula is defined as a dimensionless value that characterizes the convective heat transfer between a fluid and a solid surface, commonly used in the context of boundary layer equations for hypersonic flow to analyze heat transfer and fluid flow is calculated using Nusselt Number = Reynolds Number*Stanton Number*Prandtl Number. To calculate Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number, you need Reynolds Number (Re), Stanton Number (St) & Prandtl Number (Pr). With our tool, you need to enter the respective value for Reynolds Number, 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.

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