Equivalent Parasite Drag Area Formula

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Flat Plate Area is the area of a flat plate having. the same drag as the subject body. Check FAQs
A=ΦfμfSwet
A - Flat Plate Area?Φf - Form Factor Drag?μf - Skin Friction Coefficient?Swet - Aircraft Wetted Area?

Equivalent Parasite Drag Area Example

With values
With units
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Here is how the Equivalent Parasite Drag Area equation looks like with Values.

Here is how the Equivalent Parasite Drag Area equation looks like with Units.

Here is how the Equivalent Parasite Drag Area equation looks like.

10.9655Edit=1.499Edit0.72Edit10.16Edit
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Equivalent Parasite Drag Area Solution

Follow our step by step solution on how to calculate Equivalent Parasite Drag Area?

FIRST Step Consider the formula
A=ΦfμfSwet
Next Step Substitute values of Variables
A=1.4990.7210.16
Next Step Prepare to Evaluate
A=1.4990.7210.16
Next Step Evaluate
A=10.9654848
LAST Step Rounding Answer
A=10.9655

Equivalent Parasite Drag Area Formula Elements

Variables
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.
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.
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 Equivalent Parasite Drag Area?

Equivalent Parasite Drag Area evaluator uses Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area to evaluate the Flat Plate Area, Equivalent Parasite Drag Area is a concept used in aerodynamics to represent the total drag of an aircraft due to non-lifting components such as the fuselage, wings, tail surfaces, and any other protruding features. It's called "equivalent" because it's a hypothetical area that, if exposed to the airstream, would produce the same amount of drag as the entire aircraft. Flat Plate Area is denoted by A symbol.

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

FAQs on Equivalent Parasite Drag Area

What is the formula to find Equivalent Parasite Drag Area?
The formula of Equivalent Parasite Drag Area is expressed as Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area. Here is an example- 10.9728 = 1.499*0.72*10.16.
How to calculate Equivalent Parasite Drag Area?
With Form Factor Drag f), Skin Friction Coefficient f) & Aircraft Wetted Area (Swet) we can find Equivalent Parasite Drag Area using the formula - Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area.
Can the Equivalent Parasite Drag Area be negative?
No, the Equivalent Parasite Drag Area, measured in Area cannot be negative.
Which unit is used to measure Equivalent Parasite Drag Area?
Equivalent Parasite Drag Area is usually measured using the Square Meter[m²] for Area. Square Kilometer[m²], Square Centimeter[m²], Square Millimeter[m²] are the few other units in which Equivalent Parasite Drag Area can be measured.
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