Overall Skin-Friction Drag Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Overall Skin-friction Drag Coefficient = 1.328/sqrt(Reynolds Number using Chord Length)
CD,f = 1.328/sqrt(Rec)
This formula uses 1 Functions, 2 Variables
Functions Used
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)
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
CD,f = 1.328/sqrt(Rec) --> 1.328/sqrt(2000)
Evaluating ... ...
CD,f = 0.0296949827411972
STEP 3: Convert Result to Output's Unit
0.0296949827411972 --> No Conversion Required
FINAL ANSWER
0.0296949827411972 0.029695 <-- Overall Skin-friction Drag Coefficient
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
Shikha Maurya has verified this Calculator and 200+ more calculators!

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 Formula

​LaTeX ​Go
Overall Skin-friction Drag Coefficient = 1.328/sqrt(Reynolds Number using Chord Length)
CD,f = 1.328/sqrt(Rec)

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 Overall Skin-Friction Drag Coefficient?

Overall Skin-Friction Drag Coefficient calculator uses Overall Skin-friction Drag Coefficient = 1.328/sqrt(Reynolds Number using Chord Length) to calculate the Overall Skin-friction Drag Coefficient, Overall Skin-Friction Drag Coefficient 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 in viscous flow conditions, commonly used in aerodynamics and fluid mechanics applications. Overall Skin-friction Drag Coefficient is denoted by CD,f symbol.

How to calculate Overall Skin-Friction Drag Coefficient using this online calculator? To use this online calculator for Overall Skin-Friction Drag Coefficient, enter Reynolds Number using Chord Length (Rec) and hit the calculate button. Here is how the Overall Skin-Friction Drag Coefficient calculation can be explained with given input values -> 0.029695 = 1.328/sqrt(2000).

FAQ

What is Overall Skin-Friction Drag Coefficient?
Overall Skin-Friction Drag Coefficient 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 in viscous flow conditions, commonly used in aerodynamics and fluid mechanics applications and is represented as CD,f = 1.328/sqrt(Rec) or Overall Skin-friction Drag Coefficient = 1.328/sqrt(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.
How to calculate Overall Skin-Friction Drag Coefficient?
Overall Skin-Friction Drag Coefficient 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 in viscous flow conditions, commonly used in aerodynamics and fluid mechanics applications is calculated using Overall Skin-friction Drag Coefficient = 1.328/sqrt(Reynolds Number using Chord Length). To calculate Overall Skin-Friction Drag Coefficient, you need Reynolds Number using Chord Length (Rec). 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 = 0.02667/(Reynolds Number using Chord Length)^0.139
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!