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Aircraft Gross Wing Area given Vehicle Stalling Speed Formula

GoAircraft 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

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

S - Aircraft Gross Wing Area?M_Aircraft - Mass Aircraft?V - Vehicle Speed?ρ - Density Altitude for flying?C_L,max - Maximum Lift Coefficient?[g] - Gravitational acceleration on Earth?

Aircraft Gross Wing Area given Vehicle Stalling Speed Example

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Here is how the Aircraft Gross Wing Area given Vehicle Stalling Speed equation looks like with Values.

Here is how the Aircraft Gross Wing Area given Vehicle Stalling Speed equation looks like with Units.

Here is how the Aircraft Gross Wing Area given Vehicle Stalling Speed equation looks like.

12.8228 = 2 \cdot 50000 \cdot \frac{9.8066}{268^{2} \cdot 1.21 \cdot 0.88}

12.8228m² = 2 \cdot 50000kg \cdot \frac{9.8066m/s²}{{268km/h}^{2} \cdot 1.21kg/m³ \cdot 0.88}

12.8228 = 2 \cdot 50000 \cdot \frac{9.8066}{268^{2} \cdot 1.21 \cdot 0.88}

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Aircraft Gross Wing Area given Vehicle Stalling Speed Solution

Follow our step by step solution on how to calculate Aircraft Gross Wing Area given Vehicle Stalling Speed?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

S = 2 \cdot 50000kg \cdot \frac{[g]}{{268km/h}^{2} \cdot 1.21kg/m³ \cdot 0.88}

Next Step Substitute values of Constants

∴

S = 2 \cdot 50000kg \cdot \frac{9.8066m/s²}{{268km/h}^{2} \cdot 1.21kg/m³ \cdot 0.88}

Next Step Prepare to Evaluate

∴

S = 2 \cdot 50000 \cdot \frac{9.8066}{268^{2} \cdot 1.21 \cdot 0.88}

Next Step Evaluate

∴

S = 12.822805211805m²

LAST Step Rounding Answer

∴

S = 12.8228m²

Aircraft Gross Wing Area given Vehicle Stalling Speed Formula Elements

Variables

Constants

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

Mass Aircraft

Mass Aircraft is the quantity of matter in a body regardless of its volume or of any forces acting on it.

Symbol: M_Aircraft

Measurement: WeightUnit: kg

Note: Value can be positive or negative.

Formulas to find Mass Aircraft

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

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

Maximum Lift Coefficient

Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack.

Symbol: C_L,max

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Maximum Lift Coefficient

Gravitational acceleration on Earth

Gravitational acceleration on Earth means that the velocity of an object in free fall will increase by 9.8 m/s2 every second.

Symbol: [g]

Value: 9.80665 m/s²

Other Formulas to find Aircraft Gross Wing Area

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

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

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}}

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 given Vehicle Stalling Speed?

Aircraft Gross Wing Area given Vehicle Stalling Speed evaluator uses Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient) to evaluate the Aircraft Gross Wing Area, Aircraft Gross Wing Area given Vehicle Stalling Speed is surface area of wing is calculated by looking at wing from 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 given Vehicle Stalling Speed using this online evaluator? To use this online evaluator for Aircraft Gross Wing Area given Vehicle Stalling Speed, enter Mass Aircraft (M_Aircraft), Vehicle Speed (V), Density Altitude for flying (ρ) & Maximum Lift Coefficient (C_L,max) and hit the calculate button.

FAQs on Aircraft Gross Wing Area given Vehicle Stalling Speed

What is the formula to find Aircraft Gross Wing Area given Vehicle Stalling Speed?

The formula of Aircraft Gross Wing Area given Vehicle Stalling Speed is expressed as Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient). Here is an example- 12.82281 = 2*50000*[g]/(74.4444444444444^2*1.21*0.88).

How to calculate Aircraft Gross Wing Area given Vehicle Stalling Speed?

With Mass Aircraft (M_Aircraft), Vehicle Speed (V), Density Altitude for flying (ρ) & Maximum Lift Coefficient (C_L,max) we can find Aircraft Gross Wing Area given Vehicle Stalling Speed using the formula - Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient). This formula also uses Gravitational acceleration on Earth constant(s).

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=Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient)
Aircraft Gross Wing Area=2*Mass Aircraft*[g]/(Density Altitude for flying*Lift Coefficient*Vehicle Speed^2)

Can the Aircraft Gross Wing Area given Vehicle Stalling Speed be negative?

Yes, the Aircraft Gross Wing Area given Vehicle Stalling Speed, measured in Area can be negative.

Which unit is used to measure Aircraft Gross Wing Area given Vehicle Stalling Speed?

Aircraft Gross Wing Area given Vehicle Stalling Speed 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 given Vehicle Stalling Speed can be measured.

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: Value
: Unit

Aircraft Gross Wing Area given Vehicle Stalling Speed Formula

​GoAircraft 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

Aircraft Gross Wing Area given Vehicle Stalling Speed Example

Aircraft Gross Wing Area given Vehicle Stalling Speed Solution

Aircraft Gross Wing Area given Vehicle Stalling Speed Formula Elements

Other Formulas to find Aircraft Gross Wing Area

Other formulas in Aircraft Gross Wing category

How to Evaluate Aircraft Gross Wing Area given Vehicle Stalling Speed?

FAQs on Aircraft Gross Wing Area given Vehicle Stalling Speed

Variable Name

GoAircraft 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