Skin Friction Coefficient given Flat Plate Area Formula

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Skin Friction Coefficient is an important dimensionless parameter in boundary-layer flows. It specifies the fraction of the local dynamic pressure. Check FAQs
μf=AΦfSwet
μf - Skin Friction Coefficient?A - Flat Plate Area?Φf - Form Factor Drag?Swet - Aircraft Wetted Area?

Skin Friction Coefficient given Flat Plate Area Example

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Here is how the Skin Friction Coefficient given Flat Plate Area equation looks like with Values.

Here is how the Skin Friction Coefficient given Flat Plate Area equation looks like with Units.

Here is how the Skin Friction Coefficient given Flat Plate Area equation looks like.

0.7203Edit=10.97Edit1.499Edit10.16Edit
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Skin Friction Coefficient given Flat Plate Area Solution

Follow our step by step solution on how to calculate Skin Friction Coefficient given Flat Plate Area?

FIRST Step Consider the formula
μf=AΦfSwet
Next Step Substitute values of Variables
μf=10.971.49910.16
Next Step Prepare to Evaluate
μf=10.971.49910.16
Next Step Evaluate
μf=0.720296470612955
LAST Step Rounding Answer
μf=0.7203

Skin Friction Coefficient given Flat Plate Area Formula Elements

Variables
Skin Friction Coefficient
Skin Friction Coefficient is an important dimensionless parameter in boundary-layer flows. It specifies the fraction of the local dynamic pressure.
Symbol: μf
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Flat Plate Area
Flat Plate Area is the area of a flat plate having. the same drag as the subject body.
Symbol: A
Measurement: AreaUnit:
Note: Value should be greater than 0.
Form Factor Drag
Form Factor Drag is the ratio between the body’s parasite drag and the skin friction drag of the equivalent plate.
Symbol: Φf
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Aircraft Wetted Area
The Aircraft Wetted Area is the surface area that interacts with the working fluid or gas.
Symbol: Swet
Measurement: AreaUnit:
Note: Value should be greater than 0.

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How to Evaluate Skin Friction Coefficient given Flat Plate Area?

Skin Friction Coefficient given Flat Plate Area evaluator uses Skin Friction Coefficient = Flat Plate Area/(Form Factor Drag*Aircraft Wetted Area) to evaluate the Skin Friction Coefficient, The Skin Friction Coefficient given Flat Plate Area is a dimensionless quantity that characterizes the frictional drag generated by the airflow along the surfaces of an aircraft, this formula is defined as quantity that specifies the fraction of the local dynamic pressure and shear stress on the body. Skin Friction Coefficient is denoted by μf symbol.

How to evaluate Skin Friction Coefficient given Flat Plate Area using this online evaluator? To use this online evaluator for Skin Friction Coefficient given Flat Plate Area, enter Flat Plate Area (A), Form Factor Drag f) & Aircraft Wetted Area (Swet) and hit the calculate button.

FAQs on Skin Friction Coefficient given Flat Plate Area

What is the formula to find Skin Friction Coefficient given Flat Plate Area?
The formula of Skin Friction Coefficient given Flat Plate Area is expressed as Skin Friction Coefficient = Flat Plate Area/(Form Factor Drag*Aircraft Wetted Area). Here is an example- 0.719816 = 10.97/(1.499*10.16).
How to calculate Skin Friction Coefficient given Flat Plate Area?
With Flat Plate Area (A), Form Factor Drag f) & Aircraft Wetted Area (Swet) we can find Skin Friction Coefficient given Flat Plate Area using the formula - Skin Friction Coefficient = Flat Plate Area/(Form Factor Drag*Aircraft Wetted Area).
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