Equivalent Parasite Drag Area Calculator

✖Form Factor Drag is the ratio between the body’s parasite drag and the skin friction drag of the equivalent plate.ⓘ Form Factor Drag [Φ_f]			+10% -10%
✖Skin Friction Coefficient is an important dimensionless parameter in boundary-layer flows. It specifies the fraction of the local dynamic pressure.ⓘ Skin Friction Coefficient [μ_f]			+10% -10%
✖The Aircraft Wetted Area is the surface area that interacts with the working fluid or gas.ⓘ Aircraft Wetted Area [S_wet]			+10% -10%

✖Flat Plate Area is the area of a flat plate having. the same drag as the subject body.ⓘ Equivalent Parasite Drag Area [A]

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Equivalent Parasite Drag Area Solution

STEP 0: Pre-Calculation Summary

Formula Used

Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area
A = Φ_f*μ_f*S_wet
This formula uses 4 Variables

Variables Used

Flat Plate Area - (Measured in Square Meter) - Flat Plate Area is the area of a flat plate having. the same drag as the subject body.
Form Factor Drag - Form Factor Drag is the ratio between the body’s parasite drag and the skin friction drag of the equivalent plate.
Skin Friction Coefficient - Skin Friction Coefficient is an important dimensionless parameter in boundary-layer flows. It specifies the fraction of the local dynamic pressure.
Aircraft Wetted Area - (Measured in Square Meter) - The Aircraft Wetted Area is the surface area that interacts with the working fluid or gas.

STEP 1: Convert Input(s) to Base Unit

Form Factor Drag: 1.499 --> No Conversion Required
Skin Friction Coefficient: 0.72 --> No Conversion Required
Aircraft Wetted Area: 10.16 Square Meter --> 10.16 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

A = Φ_f*μ_f*S_wet --> 1.499*0.72*10.16

Evaluating ... ...

A = 10.9654848

STEP 3: Convert Result to Output's Unit

10.9654848 Square Meter --> No Conversion Required

FINAL ANSWER

10.9654848 ≈ 10.96548 Square Meter <-- Flat Plate Area

(Calculation completed in 00.004 seconds)

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National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

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Equivalent Parasite Drag Area Formula

LaTeX Go

Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area
A = Φ_f*μ_f*S_wet

What is flat plate?

A flat plate is geometrically the simplest airfoil one can think of. In spite of its simplicity, its aerodynamic behavior can give significant values and im- plications to design and validation of computational or experimental models.

How to Calculate Equivalent Parasite Drag Area?

Equivalent Parasite Drag Area calculator uses Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area to calculate 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 calculate Equivalent Parasite Drag Area using this online calculator? To use this online calculator for Equivalent Parasite Drag Area, enter Form Factor Drag (Φ_f), Skin Friction Coefficient (μ_f) & Aircraft Wetted Area (S_wet) and hit the calculate button. Here is how the Equivalent Parasite Drag Area calculation can be explained with given input values -> 10.9728 = 1.499*0.72*10.16.

FAQ

What is Equivalent Parasite Drag 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 and is represented as A = Φ_f*μ_f*S_wet or Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area. Form Factor Drag is the ratio between the body’s parasite drag and the skin friction drag of the equivalent plate, Skin Friction Coefficient is an important dimensionless parameter in boundary-layer flows. It specifies the fraction of the local dynamic pressure & The Aircraft Wetted Area is the surface area that interacts with the working fluid or gas.

How to calculate Equivalent Parasite Drag 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 is calculated using Flat Plate Area = Form Factor Drag*Skin Friction Coefficient*Aircraft Wetted Area. To calculate Equivalent Parasite Drag Area, you need Form Factor Drag (Φ_f), Skin Friction Coefficient (μ_f) & Aircraft Wetted Area (S_wet). With our tool, you need to enter the respective value for Form Factor Drag, Skin Friction Coefficient & Aircraft Wetted Area and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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