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

✖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.ⓘ Lifting Force of Aircraft [L_Aircraft]			+10% -10%
✖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.ⓘ Density Altitude for flying [ρ]			+10% -10%
✖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.ⓘ Vehicle Speed [V]			+10% -10%
✖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.ⓘ Lift Coefficient [C_l]			+10% -10%

✖Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing.ⓘ Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle [S]

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

STEP 0: Pre-Calculation Summary

Formula Used

Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient)
S = L_Aircraft/(0.5*ρ*V^2*C_l)
This formula uses 5 Variables

Variables Used

Aircraft Gross Wing Area - (Measured in Square Meter) - Aircraft Gross Wing Area calculated by looking at the wing from a top-down view and measuring the area of the wing.
Lifting Force of Aircraft - (Measured in Kilonewton) - 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.
Density Altitude for flying - (Measured in Kilogram per Cubic Meter) - 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.
Vehicle Speed - (Measured in Kilometer per Hour) - 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.
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.

STEP 1: Convert Input(s) to Base Unit

Lifting Force of Aircraft: 1072.39 Kilonewton --> 1072.39 Kilonewton No Conversion Required
Density Altitude for flying: 1.21 Kilogram per Cubic Meter --> 1.21 Kilogram per Cubic Meter No Conversion Required
Vehicle Speed: 268 Kilometer per Hour --> 268 Kilometer per Hour No Conversion Required
Lift Coefficient: 0.001 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

S = L_Aircraft/(0.5*ρ*V^2*C_l) --> 1072.39/(0.5*1.21*268^2*0.001)

Evaluating ... ...

S = 24.6790133457543

STEP 3: Convert Result to Output's Unit

24.6790133457543 Square Meter --> No Conversion Required

FINAL ANSWER

24.6790133457543 ≈ 24.67901 Square Meter <-- Aircraft Gross Wing Area

(Calculation completed in 00.020 seconds)

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Created by Mithila Muthamma PA

Coorg Institute of Technology (CIT), Coorg

Mithila Muthamma PA has created this Calculator and 2000+ more calculators!

Verified by M Naveen

National Institute of Technology (NIT), Warangal

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< Aircraft Gross Wing Calculators

Vehicle Stalling Speed given Maximum Attainable Lift Coefficient

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

Maximum Attainable Lift Coefficient given Vehicle Stalling Speed

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

Aircraft Gross Wing Area given Vehicle Speed under Steady Flight Conditions

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

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

LaTeX Go Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient)

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

LaTeX Go

Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient)
S = L_Aircraft/(0.5*ρ*V^2*C_l)

What is Lift force?

Lift is the force that directly opposes the weight of an airplane and holds the airplane in the air. Lift is a mechanical aerodynamic force produced by the motion of the airplane through the air. Because lift is a force, it is a vector quantity, having both a magnitude and a direction associated with it.

What is gross wing area ?

The wing area is a projected area and is almost half of the total surface area. Aspect ratio is a measure of how long and slender a wing is from tip to tip. The Aspect Ratio of a wing is defined to be the square of the span divided by the wing area and is given the symbol AR.

How to Calculate 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 calculator uses Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient) to calculate 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 calculate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle using this online calculator? To use this online calculator 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. Here is how the Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle calculation can be explained with given input values -> 24.67901 = 1072390/(0.5*1.21*74.4444444444444^2*0.001).

FAQ

What is 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 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 and is represented as S = L_Aircraft/(0.5*ρ*V^2*C_l) or Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient). 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, 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, 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 & 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.

How to calculate 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 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 is calculated using Aircraft Gross Wing Area = Lifting Force of Aircraft/(0.5*Density Altitude for flying*Vehicle Speed^2*Lift Coefficient). To calculate Aircraft Gross Wing Area for Lifting Force Provided by Wing Body of Vehicle, you need Lifting Force of Aircraft (L_Aircraft), Density Altitude for flying (ρ), Vehicle Speed (V) & Lift Coefficient (C_l). With our tool, you need to enter the respective value for Lifting Force of Aircraft, Density Altitude for flying, Vehicle Speed & Lift Coefficient and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Aircraft Gross Wing Area?

In this formula, Aircraft Gross Wing Area uses Lifting Force of Aircraft, Density Altitude for flying, Vehicle Speed & Lift Coefficient. We can use 2 other way(s) to calculate the same, which is/are as follows -

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)

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