Aircraft Gross Wing Area given Vehicle Stalling Speed Calculator

✖Mass Aircraft is the quantity of matter in a body regardless of its volume or of any forces acting on it.ⓘ Mass Aircraft [M_Aircraft]			+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%
✖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%
✖Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack.ⓘ Maximum Lift Coefficient [C_L,max]			+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 given Vehicle Stalling Speed [S]

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Aircraft Gross Wing Area given Vehicle Stalling Speed Solution

STEP 0: Pre-Calculation Summary

Formula Used

Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient)
S = 2*M_Aircraft*[g]/(V^2*ρ*C_L,max)
This formula uses 1 Constants, 5 Variables

Constants Used

[g] - Gravitational acceleration on Earth Value Taken As 9.80665

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.
Mass Aircraft - (Measured in Kilogram) - Mass Aircraft is the quantity of matter in a body regardless of its volume or of any forces acting on it.
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.
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.
Maximum Lift Coefficient - Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack.

STEP 1: Convert Input(s) to Base Unit

Mass Aircraft: 50000 Kilogram --> 50000 Kilogram No Conversion Required
Vehicle Speed: 268 Kilometer per Hour --> 268 Kilometer per Hour No Conversion Required
Density Altitude for flying: 1.21 Kilogram per Cubic Meter --> 1.21 Kilogram per Cubic Meter No Conversion Required
Maximum Lift Coefficient: 0.88 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

S = 2*M_Aircraft*[g]/(V^2*ρ*C_L,max) --> 2*50000*[g]/(268^2*1.21*0.88)

Evaluating ... ...

S = 12.822805211805

STEP 3: Convert Result to Output's Unit

12.822805211805 Square Meter --> No Conversion Required

FINAL ANSWER

12.822805211805 ≈ 12.82281 Square Meter <-- Aircraft Gross Wing Area

(Calculation completed in 00.004 seconds)

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Created by Mithila Muthamma PA

Coorg Institute of Technology (CIT), Coorg

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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 given Vehicle Stalling Speed Formula

LaTeX Go

Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient)
S = 2*M_Aircraft*[g]/(V^2*ρ*C_L,max)

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.

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

Aircraft Gross Wing Area given Vehicle Stalling Speed calculator uses Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient) to calculate 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 calculate Aircraft Gross Wing Area given Vehicle Stalling Speed using this online calculator? To use this online calculator 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. Here is how the Aircraft Gross Wing Area given Vehicle Stalling Speed calculation can be explained with given input values -> 12.82281 = 2*50000*[g]/(74.4444444444444^2*1.21*0.88).

FAQ

What is Aircraft Gross Wing Area given Vehicle Stalling Speed?

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 and is represented as S = 2*M_Aircraft*[g]/(V^2*ρ*C_L,max) or Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient). Mass Aircraft is the quantity of matter in a body regardless of its volume or of any forces acting on it, 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, 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 & Maximum Lift Coefficient is defined as the lift coefficient of the airfoil at stalling angle of attack.

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

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 is calculated using Aircraft Gross Wing Area = 2*Mass Aircraft*[g]/(Vehicle Speed^2*Density Altitude for flying*Maximum Lift Coefficient). To calculate Aircraft Gross Wing Area given Vehicle Stalling Speed, you need Mass Aircraft (M_Aircraft), Vehicle Speed (V), Density Altitude for flying (ρ) & Maximum Lift Coefficient (C_L,max). With our tool, you need to enter the respective value for Mass Aircraft, Vehicle Speed, Density Altitude for flying & Maximum 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 Mass Aircraft, Vehicle Speed, Density Altitude for flying & Maximum Lift Coefficient. We can use 2 other way(s) to calculate the same, which is/are as follows -

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)

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