Overall Skin-Friction Drag Coefficient for Incompressible Flow Calculator

✖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 using Chord Length [Re_c]

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✖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 for Incompressible Flow [C_D,f]

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Overall Skin-Friction Drag Coefficient for Incompressible Flow Solution

STEP 0: Pre-Calculation Summary

Formula Used

Overall Skin-friction Drag Coefficient = 0.02667/(Reynolds Number using Chord Length)^0.139
C_D,f = 0.02667/(Re_c)^0.139
This formula uses 2 Variables

Variables Used

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.
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.

STEP 1: Convert Input(s) to Base Unit

Reynolds Number using Chord Length: 2000 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_D,f = 0.02667/(Re_c)^0.139 --> 0.02667/(2000)^0.139

Evaluating ... ...

C_D,f = 0.00927213713649144

STEP 3: Convert Result to Output's Unit

0.00927213713649144 --> No Conversion Required

FINAL ANSWER

0.00927213713649144 ≈ 0.009272 <-- Overall Skin-friction Drag Coefficient

(Calculation completed in 00.004 seconds)

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Home » Engineering » Mechanical » Fluid Mechanics » Hypersonic Flow » Flat Plate for Viscous Flow Case » Reference Temperature Method » Overall Skin-Friction Drag Coefficient for Incompressible Flow

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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< Reference Temperature Method Calculators

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

Overall Skin-Friction Drag Coefficient for Incompressible Flow Formula

LaTeX Go

Overall Skin-friction Drag Coefficient = 0.02667/(Reynolds Number using Chord Length)^0.139
C_D,f = 0.02667/(Re_c)^0.139

What is a Local Reynolds Number?

Based on these observations and the energy equation of a disturbed fluid element, a local Reynolds number Re L is derived to represent the maximum ratio of the energy supplement to the energy dissipation in a cross-section.

How to Calculate Overall Skin-Friction Drag Coefficient for Incompressible Flow?

Overall Skin-Friction Drag Coefficient for Incompressible Flow calculator uses Overall Skin-friction Drag Coefficient = 0.02667/(Reynolds Number using Chord Length)^0.139 to calculate the Overall Skin-friction Drag Coefficient, Overall Skin-Friction Drag Coefficient for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force exerted by a fluid on a flat plate, providing a measure of the resistance to fluid flow over the plate's surface in incompressible flow conditions. Overall Skin-friction Drag Coefficient is denoted by C_D,f symbol.

How to calculate Overall Skin-Friction Drag Coefficient for Incompressible Flow using this online calculator? To use this online calculator for Overall Skin-Friction Drag Coefficient for Incompressible Flow, enter Reynolds Number using Chord Length (Re_c) and hit the calculate button. Here is how the Overall Skin-Friction Drag Coefficient for Incompressible Flow calculation can be explained with given input values -> 0.009272 = 0.02667/(2000)^0.139.

FAQ

What is Overall Skin-Friction Drag Coefficient for Incompressible Flow?

Overall Skin-Friction Drag Coefficient for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force exerted by a fluid on a flat plate, providing a measure of the resistance to fluid flow over the plate's surface in incompressible flow conditions and is represented as C_D,f = 0.02667/(Re_c)^0.139 or Overall Skin-friction Drag Coefficient = 0.02667/(Reynolds Number using Chord Length)^0.139. 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.

How to calculate Overall Skin-Friction Drag Coefficient for Incompressible Flow?

Overall Skin-Friction Drag Coefficient for Incompressible Flow formula is defined as a dimensionless quantity that characterizes the frictional force exerted by a fluid on a flat plate, providing a measure of the resistance to fluid flow over the plate's surface in incompressible flow conditions is calculated using Overall Skin-friction Drag Coefficient = 0.02667/(Reynolds Number using Chord Length)^0.139. To calculate Overall Skin-Friction Drag Coefficient for Incompressible Flow, you need Reynolds Number using Chord Length (Re_c). With our tool, you need to enter the respective value for Reynolds Number using Chord Length 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 Overall Skin-friction Drag Coefficient?

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

Overall Skin-friction Drag Coefficient = 1.328/sqrt(Reynolds Number using Chord Length)

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