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Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Formula

GoAircraft Gross Wing Area given Vehicle Speed under Steady Flight Conditions Formula

GoAircraft Gross Wing Area given Vehicle Stalling Speed Formula

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Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing. Check FAQs

S = \frac{L Aircraft}{0.5 \cdot ρ \cdot V^{2} \cdot C l}

S - Aircraft Gross Wing Area?L_Aircraft - Lifting Force of Aircraft?ρ - Density Altitude for flying?V - Vehicle Speed?C_l - Lift Coefficient?

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Example

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Here is how the Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle equation looks like with Values.

Here is how the Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle equation looks like with Units.

Here is how the Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle equation looks like.

24.679 = \frac{1072.39}{0.5 \cdot 1.21 \cdot 268^{2} \cdot 0.001}

24.679m² = \frac{1072.39kN}{0.5 \cdot 1.21kg/m³ \cdot {268km/h}^{2} \cdot 0.001}

24.679 = \frac{1072.39}{0.5 \cdot 1.21 \cdot 268^{2} \cdot 0.001}

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Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Solution

Follow our step by step solution on how to calculate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle?

FIRST Step Consider the formula

S = \frac{L Aircraft}{0.5 \cdot ρ \cdot V^{2} \cdot C l}

Next Step Substitute values of Variables

∴

S = \frac{1072.39kN}{0.5 \cdot 1.21kg/m³ \cdot {268km/h}^{2} \cdot 0.001}

Next Step Prepare to Evaluate

∴

S = \frac{1072.39}{0.5 \cdot 1.21 \cdot 268^{2} \cdot 0.001}

Next Step Evaluate

∴

S = 24.6790133457543m²

LAST Step Rounding Answer

∴

S = 24.679m²

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Formula Elements

Variables

Aircraft Gross Wing Area

Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing.

Symbol: S

Measurement: AreaUnit: m²

Note: Value can be positive or negative.

Formulas to find Aircraft Gross Wing Area

Lifting Force of Aircraft

Lifting Force of Aircraft provided by the wing-body of the vehicle. Lift is defined as the component of the aerodynamic force that is perpendicular to the flow direction.

Symbol: L_Aircraft

Measurement: ForceUnit: kN

Note: Value can be positive or negative.

Formulas to find Lifting Force of Aircraft

Density Altitude for flying

Density Altitude for flying is a representation of the amount of mass of a substance, material or object in relation to the space it occupies at an altitude.

Symbol: ρ

Measurement: DensityUnit: kg/m³

Note: Value can be positive or negative.

Formulas to find Density Altitude for flying

Vehicle Speed

Vehicle Speed (True Air Speed) of an aircraft is the speed of aircraft relative to air mass through which it is flying. The true airspeed is important information for accurate navigation of aircraft.

Symbol: V

Measurement: SpeedUnit: km/h

Note: Value can be positive or negative.

Formulas to find Vehicle Speed

Lift Coefficient

The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

Symbol: C_l

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Lift Coefficient

Other Formulas to find Aircraft Gross Wing Area

Go Aircraft Gross Wing Area given Vehicle Speed under Steady Flight Conditions

S = 2 \cdot M Aircraft \cdot \frac{[g]}{ρ \cdot C l \cdot V^{2}}

Go Aircraft Gross Wing Area given Vehicle Stalling Speed

S = 2 \cdot M Aircraft \cdot \frac{[g]}{V^{2} \cdot ρ \cdot C L,max}

Other formulas in Aircraft Gross Wing category

Go Vehicle Stalling Speed given Maximum Attainable Lift Coefficient

V = \sqrt{\frac{2 \cdot M Aircraft \cdot [g]}{ρ \cdot S \cdot C L,max}}

Go Maximum Attainable Lift Coefficient given Vehicle Stalling Speed

C L,max = 2 \cdot M Aircraft \cdot \frac{[g]}{ρ \cdot S \cdot V^{2}}

How to Evaluate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle?

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle evaluator uses Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient) to evaluate the Aircraft Gross Wing Area, Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicleis a projected area and is almost half of total surface area. surface area of a wing is calculated by looking at wing from a top-down view and measuring area of wing. This surface area is also known as planform area. Aircraft Gross Wing Area is denoted by S symbol.

How to evaluate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle using this online evaluator? To use this online evaluator for Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle, enter Lifting Force of Aircraft (L_Aircraft), Density Altitude for flying (ρ), Vehicle Speed (V) & Lift Coefficient (C_l) and hit the calculate button.

FAQs on Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle

What is the formula to find Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle?

The formula of Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle is expressed as Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient). Here is an example- 24.67901 = 1072390/(0.5*1.21*74.4444444444444^2*0.001).

How to calculate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle?

With Lifting Force of Aircraft (L_Aircraft), Density Altitude for flying (ρ), Vehicle Speed (V) & Lift Coefficient (C_l) we can find Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle using the formula - Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient).

What are the other ways to Calculate Aircraft Gross Wing Area?

Here are the different ways to Calculate Aircraft Gross Wing Area-

Aircraft Gross Wing Area=2*Mass Aircraft*[g]/(Density Altitude for flying*Lift Coefficient*Vehicle Speed^2)
Aircraft Gross Wing Area=2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient)

Can the Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle be negative?

Yes, the Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle, measured in Area can be negative.

Which unit is used to measure Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle?

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle 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 Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle can be measured.

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Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Formula

​GoAircraft Gross Wing Area given Vehicle Speed under Steady Flight Conditions Formula

​GoAircraft Gross Wing Area given Vehicle Stalling Speed Formula

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Example

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Solution

Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle Formula Elements

Other Formulas to find Aircraft Gross Wing Area

Other formulas in Aircraft Gross Wing category

How to Evaluate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle?

FAQs on Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle

Variable Name

GoAircraft Gross Wing Area given Vehicle Speed under Steady Flight Conditions Formula

GoAircraft Gross Wing Area given Vehicle Stalling Speed Formula