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Lifting Force Provided by Wing Body of Vehicle Formula

GoLifting Force given Friction Force due to Rolling Resistance Formula

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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. Check FAQs

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

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

Lifting Force Provided by Wing Body of Vehicle Example

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

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

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

999.431 = 0.5 \cdot 1.21 \cdot 268^{2} \cdot 23 \cdot 0.001

999.431kN = 0.5 \cdot 1.21kg/m³ \cdot {268km/h}^{2} \cdot 23m² \cdot 0.001

999.431 = 0.5 \cdot 1.21 \cdot 268^{2} \cdot 23 \cdot 0.001

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Lifting Force Provided by Wing Body of Vehicle Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

L Aircraft = 0.5 \cdot 1.21kg/m³ \cdot {268km/h}^{2} \cdot 23m² \cdot 0.001

Next Step Prepare to Evaluate

∴

L Aircraft = 0.5 \cdot 1.21 \cdot 268^{2} \cdot 23 \cdot 0.001

Next Step Evaluate

∴

L Aircraft = 999430.96N

Next Step Convert to Output's Unit

∴

L Aircraft = 999.43096kN

LAST Step Rounding Answer

∴

L Aircraft = 999.431kN

Lifting Force Provided by Wing Body of Vehicle Formula Elements

Variables

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

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

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 Lifting Force of Aircraft

Go Lifting Force given Friction Force due to Rolling Resistance

L Aircraft = (((M Aircraft \cdot [g] \cdot \cos (Φ)) - (\frac{F Friction}{μ r})))

Other formulas in Aircraft Runway Length Estimation category

Go Desired Take off Weight

D = PYL + OEW + FW

Go Payload carried when desired take-off weight is considered

PYL = D - OEW - FW

Go Operating Empty Weight when Desired Take-off Weight is considered

OEW = D - PYL - FW

Go Fuel Weight to be Carried given Desired Takeoff Weight

FW = D - PYL - OEW

How to Evaluate Lifting Force Provided by Wing Body of Vehicle?

Lifting Force Provided by Wing Body of Vehicle evaluator uses Lifting Force of Aircraft = 0.5*Density Altitude for flying*Vehicle Speed^2*Aircraft Gross Wing Area*Lift Coefficient to evaluate the Lifting Force of Aircraft, Lifting Force Provided by Wing Body of Vehicle is perpendicular to the oncoming flow direction is defined as the total force provided by the wing body of the vehicle. Lifting Force of Aircraft is denoted by L_Aircraft symbol.

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

FAQs on Lifting Force Provided by Wing Body of Vehicle

What is the formula to find Lifting Force Provided by Wing Body of Vehicle?

The formula of Lifting Force Provided by Wing Body of Vehicle is expressed as Lifting Force of Aircraft = 0.5*Density Altitude for flying*Vehicle Speed^2*Aircraft Gross Wing Area*Lift Coefficient. Here is an example- 0.999431 = 0.5*1.21*74.4444444444444^2*23*0.001.

How to calculate Lifting Force Provided by Wing Body of Vehicle?

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

What are the other ways to Calculate Lifting Force of Aircraft?

Here are the different ways to Calculate Lifting Force of Aircraft-

Lifting Force of Aircraft=(((Mass Aircraft*[g]*cos(Angle between Runway and Horizontal Plane))-(Force of Friction/Coefficient of Rolling Friction)))

Can the Lifting Force Provided by Wing Body of Vehicle be negative?

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

Which unit is used to measure Lifting Force Provided by Wing Body of Vehicle?

Lifting Force Provided by Wing Body of Vehicle is usually measured using the Kilonewton[kN] for Force. Newton[kN], Exanewton[kN], Meganewton[kN] are the few other units in which Lifting Force Provided by Wing Body of Vehicle can be measured.

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Lifting Force Provided by Wing Body of Vehicle Formula

​GoLifting Force given Friction Force due to Rolling Resistance Formula

Lifting Force Provided by Wing Body of Vehicle Example

Lifting Force Provided by Wing Body of Vehicle Solution

Lifting Force Provided by Wing Body of Vehicle Formula Elements

Other Formulas to find Lifting Force of Aircraft

Other formulas in Aircraft Runway Length Estimation category

How to Evaluate Lifting Force Provided by Wing Body of Vehicle?

FAQs on Lifting Force Provided by Wing Body of Vehicle

Variable Name

GoLifting Force given Friction Force due to Rolling Resistance Formula