FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Wetted Area given Flat Plate Area Formula

GoWetted Area given Aspect Ratio Formula

Fx Copy

LaTeX Copy

The Aircraft Wetted Area is the surface area that interacts with the working fluid or gas. Check FAQs

S wet = \frac{A}{Φ f \cdot μ f}

S_wet - Aircraft Wetted Area?A - Flat Plate Area?Φ_f - Form Factor Drag?μ_f - Skin Friction Coefficient?

Wetted Area given Flat Plate Area Example

With values

With units

Only example

Here is how the Wetted Area given Flat Plate Area equation looks like with Values.

Here is how the Wetted Area given Flat Plate Area equation looks like with Units.

Here is how the Wetted Area given Flat Plate Area equation looks like.

10.1642 = \frac{10.97}{1.499 \cdot 0.72}

10.1642m² = \frac{10.97m²}{1.499 \cdot 0.72}

10.1642 = \frac{10.97}{1.499 \cdot 0.72}

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Physics » Category

Aerospace » Category

Aircraft Mechanics » fx Wetted Area given Flat Plate Area

Wetted Area given Flat Plate Area Solution

Follow our step by step solution on how to calculate Wetted Area given Flat Plate Area?

FIRST Step Consider the formula

S wet = \frac{A}{Φ f \cdot μ f}

Next Step Substitute values of Variables

∴

S wet = \frac{10.97m²}{1.499 \cdot 0.72}

Next Step Prepare to Evaluate

∴

S wet = \frac{10.97}{1.499 \cdot 0.72}

Next Step Evaluate

∴

S wet = 10.1641835297606m²

LAST Step Rounding Answer

∴

S wet = 10.1642m²

Wetted Area given Flat Plate Area Formula Elements

Variables

Aircraft Wetted Area

The Aircraft Wetted Area is the surface area that interacts with the working fluid or gas.

Symbol: S_wet

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Aircraft Wetted Area

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: m²

Note: Value should be greater than 0.

Formulas to find Flat Plate Area

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: Φ_f

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Form Factor Drag

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: μ_f

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Skin Friction Coefficient

Other Formulas to find Aircraft Wetted Area

Go Wetted Area given Aspect Ratio

S wet = \frac{{b W}^{2}}{AR w}

Other formulas in Aerodynamic Design category

Go Aerofoil Thickness for 4 Digit Series

y t = \frac{t \cdot (0.2969 \cdot x^{0.5} - 0.1260 \cdot x - 0.3516 \cdot x^{2} + 0.2843 \cdot x^{3} - 0.1015 \cdot x^{4})}{0.2}

Go Thrust-to-Weight Ratio given Minimum Coefficient of Drag

TW = (\frac{C Dmin}{W S} + k \cdot {(\frac{n}{q})}^{2} \cdot W S) \cdot q

Go Taper Ratio of Airfoil

Λ = \frac{C tip}{C root}

Go Tip Speed Ratio with Blade Number

λ = \frac{4 \cdot π}{N}

How to Evaluate Wetted Area given Flat Plate Area?

Wetted Area given Flat Plate Area evaluator uses Aircraft Wetted Area = Flat Plate Area/(Form Factor Drag*Skin Friction Coefficient) to evaluate the Aircraft Wetted Area, The Wetted Area given Flat Plate Area formula is defined as the total surface area of the aircraft that is in contact with the air during flight. It is also defined as the area that is affected by the drag of the air of an aircraft in presence of the form factor and skin friction coefficient. Aircraft Wetted Area is denoted by S_wet symbol.

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

FAQs on Wetted Area given Flat Plate Area

What is the formula to find Wetted Area given Flat Plate Area?

The formula of Wetted Area given Flat Plate Area is expressed as Aircraft Wetted Area = Flat Plate Area/(Form Factor Drag*Skin Friction Coefficient). Here is an example- 10.16418 = 10.97/(1.499*0.72).

How to calculate Wetted Area given Flat Plate Area?

With Flat Plate Area (A), Form Factor Drag (Φ_f) & Skin Friction Coefficient (μ_f) we can find Wetted Area given Flat Plate Area using the formula - Aircraft Wetted Area = Flat Plate Area/(Form Factor Drag*Skin Friction Coefficient).

What are the other ways to Calculate Aircraft Wetted Area?

Here are the different ways to Calculate Aircraft Wetted Area-

Aircraft Wetted Area=Lateral Plane Span^2/Aspect Ratio in Lateral Plane

Can the Wetted Area given Flat Plate Area be negative?

No, the Wetted Area given Flat Plate Area, measured in Area cannot be negative.

Which unit is used to measure Wetted Area given Flat Plate Area?

Wetted Area given Flat Plate 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 Wetted Area given Flat Plate Area can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

: Value
: Unit

Wetted Area given Flat Plate Area Formula

​GoWetted Area given Aspect Ratio Formula

Wetted Area given Flat Plate Area Example

Wetted Area given Flat Plate Area Solution

Wetted Area given Flat Plate Area Formula Elements

Other Formulas to find Aircraft Wetted Area

Other formulas in Aerodynamic Design category

How to Evaluate Wetted Area given Flat Plate Area?

FAQs on Wetted Area given Flat Plate Area

Variable Name

GoWetted Area given Aspect Ratio Formula