Range of Aircraft in Aircraft Design Formulas

Range of Aircraft is defined as the total distance (measured with respect to ground) traversed by the aircraft on a tank of fuel. And is denoted by R. Range of Aircraft is usually measured using the Kilometer for Length. Note that the value of Range of Aircraft is always positive.

Formulas to find Range of Aircraft in Aircraft Design

fxOptimum Range for Jet Aircraft in Cruising PhaseGo

fxHelicopter Flying RangeGo

Aircraft Design formulas that make use of Range of Aircraft

fxVelocity for Maximizing Range given Range for Jet AircraftGo

List of variables in Aircraft Design formulas

fx Velocity at Maximum Lift to Drag Ratio Go

fx Maximum Lift-to-Drag Ratio of Aircraft Go

fx Power Specific Fuel Consumption Go

fx Weight of Aircraft at Beginning of Cruise Phase Go

fx Weight of Aircraft at End of Cruise Phase Go

fx Weight of Fuel Go

fx Aircraft Weight Go

fx Lift Coefficient Go

fx Drag Coefficient Go

fx Rotor Efficiency Go

fx Coefficient of Power loss Go

FAQ

What is the Range of Aircraft?

Range of Aircraft is defined as the total distance (measured with respect to ground) traversed by the aircraft on a tank of fuel. Range of Aircraft is usually measured using the Kilometer for Length. Note that the value of Range of Aircraft is always positive.

Can the Range of Aircraft be negative?

No, the Range of Aircraft, measured in Length cannot be negative.

What unit is used to measure Range of Aircraft?

Range of Aircraft is usually measured using the Kilometer[km] for Length. Meter[km], Millimeter[km], Decimeter[km] are the few other units in which Range of Aircraft can be measured.

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