Lifting Force of Aircraft in Aircraft Runway Length Estimation Formulas

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. And is denoted by L_Aircraft. Lifting Force of Aircraft is usually measured using the Kilonewton for Force. Note that the value of Lifting Force of Aircraft is always negative.

Formulas to find Lifting Force of Aircraft in Aircraft Runway Length Estimation

fxLifting Force Provided by Wing Body of VehicleGo

fxLifting Force given Friction Force due to Rolling ResistanceGo

Aircraft Runway Length Estimation formulas that make use of Lifting Force of Aircraft

fxVehicle Speed for Lifting Force Provided by Wing Body of VehicleGo

fxLift Coefficient for Lifting Force Provided by Wing Body of VehicleGo

fxAircraft Gross Wing Area for Lifting Force Provided by Wing Body of VehicleGo

List of variables in Aircraft Runway Length Estimation formulas

fx Density Altitude for flying Go

fx Vehicle Speed Go

fx Aircraft Gross Wing Area Go

fx Lift Coefficient Go

fx Mass Aircraft Go

fx Angle between Runway and Horizontal Plane Go

fx Force of Friction Go

fx Coefficient of Rolling Friction Go

FAQ

What is the 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. Lifting Force of Aircraft is usually measured using the Kilonewton for Force. Note that the value of Lifting Force of Aircraft is always negative.

Can the Lifting Force of Aircraft be negative?

Yes, the Lifting Force of Aircraft, measured in Force can be negative.

What unit is used to measure Lifting Force of Aircraft?

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

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