Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient Calculator

✖The Overall Skin-friction Drag Coefficient is a dimensionless number representing the resistance experienced by a flat plate in hypersonic flow due to viscous effects.ⓘ Overall Skin-friction Drag Coefficient [C_D,f]

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✖The Reynolds Number using Chord Length is a dimensionless quantity that helps predict flow patterns in fluid dynamics, particularly for hypersonic flow over flat plates.ⓘ Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient [Re_c]

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Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient Solution

STEP 0: Pre-Calculation Summary

Formula Used

Reynolds Number using Chord Length = (1.328/Overall Skin-friction Drag Coefficient)^2
Re_c = (1.328/C_D,f)^2
This formula uses 2 Variables

Variables Used

Reynolds Number using Chord Length - The Reynolds Number using Chord Length is a dimensionless quantity that helps predict flow patterns in fluid dynamics, particularly for hypersonic flow over flat plates.
Overall Skin-friction Drag Coefficient - The Overall Skin-friction Drag Coefficient is a dimensionless number representing the resistance experienced by a flat plate in hypersonic flow due to viscous effects.

STEP 1: Convert Input(s) to Base Unit

Overall Skin-friction Drag Coefficient: 0.029695 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

Re_c = (1.328/C_D,f)^2 --> (1.328/0.029695)^2

Evaluating ... ...

Re_c = 1999.99767519141

STEP 3: Convert Result to Output's Unit

1999.99767519141 --> No Conversion Required

FINAL ANSWER

1999.99767519141 ≈ 1999.998 <-- Reynolds Number using Chord Length

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

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Static Velocity of Plate using Chord Length for Flat Plate Case

LaTeX Go Static Velocity = (Reynolds Number using Chord Length*Static Viscosity)/(Static Density*Chord Length)

Static Density of Plate using Chord Length for Flat Plate Case

LaTeX Go Static Density = (Reynolds Number using Chord Length*Static Viscosity)/(Static Velocity*Chord Length)

Reynolds Number for Chord Length

LaTeX Go Reynolds Number using Chord Length = Static Density*Static Velocity*Chord Length/Static Viscosity

Local Reynolds Number

LaTeX Go Local Reynolds Number = ((1.328)/Local Skin-Friction Coefficient)^2

Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient Formula

LaTeX Go

Reynolds Number using Chord Length = (1.328/Overall Skin-friction Drag Coefficient)^2
Re_c = (1.328/C_D,f)^2

What is a 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 Chord Length using Overall Skin-Friction Drag Coefficient?

Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient calculator uses Reynolds Number using Chord Length = (1.328/Overall Skin-friction Drag Coefficient)^2 to calculate the Reynolds Number using Chord Length, Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient formula is defined as a dimensionless value that characterizes fluid flow, particularly in flat plate viscous flow cases, providing a crucial parameter in understanding and analyzing fluid dynamics and drag forces. Reynolds Number using Chord Length is denoted by Re_c symbol.

How to calculate Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient using this online calculator? To use this online calculator for Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient, enter Overall Skin-friction Drag Coefficient (C_D,f) and hit the calculate button. Here is how the Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient calculation can be explained with given input values -> 3.928679 = (1.328/0.029695)^2.

FAQ

What is Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient?

Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient formula is defined as a dimensionless value that characterizes fluid flow, particularly in flat plate viscous flow cases, providing a crucial parameter in understanding and analyzing fluid dynamics and drag forces and is represented as Re_c = (1.328/C_D,f)^2 or Reynolds Number using Chord Length = (1.328/Overall Skin-friction Drag Coefficient)^2. The Overall Skin-friction Drag Coefficient is a dimensionless number representing the resistance experienced by a flat plate in hypersonic flow due to viscous effects.

How to calculate Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient?

Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient formula is defined as a dimensionless value that characterizes fluid flow, particularly in flat plate viscous flow cases, providing a crucial parameter in understanding and analyzing fluid dynamics and drag forces is calculated using Reynolds Number using Chord Length = (1.328/Overall Skin-friction Drag Coefficient)^2. To calculate Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient, you need Overall Skin-friction Drag Coefficient (C_D,f). With our tool, you need to enter the respective value for Overall Skin-friction Drag Coefficient and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Reynolds Number using Chord Length?

In this formula, Reynolds Number using Chord Length uses Overall Skin-friction Drag Coefficient. We can use 1 other way(s) to calculate the same, which is/are as follows -

Reynolds Number using Chord Length = Static Density*Static Velocity*Chord Length/Static Viscosity

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