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

✖The Nusselt Number is a dimensionless quantity that characterizes the convective heat transfer between a surface and a fluid in hypersonic flow conditions.ⓘ Nusselt Number [N_u]			+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 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 Prandtl Number is a dimensionless quantity used to characterize the ratio of momentum diffusivity to thermal diffusivity in a fluid.ⓘ Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number [Pr]

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

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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

STEP 1: Convert Input(s) to Base Unit

Nusselt Number: 1400 --> No Conversion Required
Stanton Number: 0.4 --> No Conversion Required
Reynolds Number: 5000 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

Pr = N_u/(St*Re) --> 1400/(0.4*5000)

Evaluating ... ...

Pr = 0.7

STEP 3: Convert Result to Output's Unit

0.7 --> No Conversion Required

FINAL ANSWER

0.7 <-- Prandtl 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

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

LaTeX Go

Prandtl Number = Nusselt Number/(Stanton Number*Reynolds Number)
Pr = N_u/(St*Re)

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

Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number calculator uses Prandtl Number = Nusselt Number/(Stanton Number*Reynolds Number) to calculate the Prandtl Number, Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number formula is defined as a dimensionless quantity that characterizes the ratio of momentum diffusivity to thermal diffusivity in a fluid, used to analyze heat transfer and fluid flow in hypersonic boundary layers, particularly in aerospace engineering applications. Prandtl Number is denoted by Pr symbol.

How to calculate Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number using this online calculator? To use this online calculator for Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number, enter Nusselt Number (N_u), Stanton Number (St) & Reynolds Number (Re) and hit the calculate button. Here is how the Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number calculation can be explained with given input values -> 0.0025 = 1400/(0.4*5000).

FAQ

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

Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number formula is defined as a dimensionless quantity that characterizes the ratio of momentum diffusivity to thermal diffusivity in a fluid, used to analyze heat transfer and fluid flow in hypersonic boundary layers, particularly in aerospace engineering applications and is represented as Pr = N_u/(St*Re) or Prandtl Number = Nusselt Number/(Stanton Number*Reynolds 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 Stanton Number is a dimensionless quantity used to characterize heat transfer and frictional drag in the boundary layer of hypersonic flow & 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.

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

Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number formula is defined as a dimensionless quantity that characterizes the ratio of momentum diffusivity to thermal diffusivity in a fluid, used to analyze heat transfer and fluid flow in hypersonic boundary layers, particularly in aerospace engineering applications is calculated using Prandtl Number = Nusselt Number/(Stanton Number*Reynolds Number). To calculate Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number, you need Nusselt Number (N_u), Stanton Number (St) & Reynolds Number (Re). With our tool, you need to enter the respective value for Nusselt Number, Stanton Number & Reynolds 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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