Lift Coefficient in Level Flight Formulas

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. And is denoted by C_L.

Formulas to find Lift Coefficient in Level Flight

fxCoefficient of Lift for given Thrust-to-Weight RatioGo

fxCoefficient of Lift for given thrust and weightGo

fxLift Coefficient given Minimum required ThrustGo

Level Flight formulas that make use of Lift Coefficient

fxLift for Level and Unaccelerated Flight at Negligible Thrust AngleGo

fxCoefficient of Drag for given Thrust-to-Weight RatioGo

fxCoefficient of Drag for given Thrust and WeightGo

fxZero-Lift Drag Coefficient for given Lift CoefficientGo

fxZero-lift drag coefficient at minimum required thrustGo

fxWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust AngleGo

fxThrust-to-weight ratioGo

fxThrust for given coefficients of lift and dragGo

fxWeight of Aircraft for given Coefficients of Lift and DragGo

fxMinimum Thrust required for given Lift CoefficientGo

fxPower required for given aerodynamic coefficientsGo

fxWeight of aircraft for given required powerGo

List of variables in Level Flight formulas

fx Drag Coefficient Go

fx Thrust-to-Weight Ratio Go

fx Weight of Body Go

fx Thrust Go

fx Oswald Efficiency Factor Go

fx Aspect Ratio of a Wing Go

fx Dynamic Pressure Go

fx Area Go

fx Zero Lift Drag Coefficient Go

Lift Coefficient in Level Flight Formulas

Formulas to find Lift Coefficient in Level Flight

Level Flight formulas that make use of Lift Coefficient

List of variables in Level Flight formulas

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