Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl 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 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 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 for given Nusselt's Number, Stanton Number and Prandtl Number [Re]

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

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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.
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.
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
Stanton Number: 0.4 --> No Conversion Required
Prandtl Number: 0.7 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

Re = N_u/(St*Pr) --> 1400/(0.4*0.7)

Evaluating ... ...

Re = 5000

STEP 3: Convert Result to Output's Unit

5000 --> No Conversion Required

FINAL ANSWER

5000 <-- Reynolds Number

(Calculation completed in 00.004 seconds)

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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

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

LaTeX Go

Reynolds Number = Nusselt Number/(Stanton Number*Prandtl Number)
Re = N_u/(St*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 Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number?

Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number calculator uses Reynolds Number = Nusselt Number/(Stanton Number*Prandtl Number) to calculate the Reynolds Number, Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number formula is defined as a dimensionless value that characterizes fluid flow, particularly in the context of boundary layer equations for hypersonic flow, providing a crucial parameter in understanding and predicting fluid behavior under extreme conditions. Reynolds Number is denoted by Re symbol.

How to calculate Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number using this online calculator? To use this online calculator for Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number, enter Nusselt Number (N_u), Stanton Number (St) & Prandtl Number (Pr) and hit the calculate button. Here is how the Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number calculation can be explained with given input values -> 17.85714 = 1400/(0.4*0.7).

FAQ

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

Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number formula is defined as a dimensionless value that characterizes fluid flow, particularly in the context of boundary layer equations for hypersonic flow, providing a crucial parameter in understanding and predicting fluid behavior under extreme conditions and is represented as Re = N_u/(St*Pr) or Reynolds Number = Nusselt Number/(Stanton 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 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 Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number?

Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number formula is defined as a dimensionless value that characterizes fluid flow, particularly in the context of boundary layer equations for hypersonic flow, providing a crucial parameter in understanding and predicting fluid behavior under extreme conditions is calculated using Reynolds Number = Nusselt Number/(Stanton Number*Prandtl Number). To calculate Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number, you need Nusselt Number (N_u), Stanton Number (St) & Prandtl Number (Pr). With our tool, you need to enter the respective value for Nusselt 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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