Optimum Range of Aircraft in Aircraft Design Formulas

Optimum 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_opt. Optimum Range of Aircraft is usually measured using the Kilometer for Length. Note that the value of Optimum Range of Aircraft is always negative.

Formulas to find Optimum Range of Aircraft in Aircraft Design

fxOptimum Range for Prop-Driven Aircraft in Cruising PhaseGo

List of variables in Aircraft Design formulas

fx Propeller Efficiency 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

FAQ

What is the Optimum Range of Aircraft?

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

Can the Optimum Range of Aircraft be negative?

Yes, the Optimum Range of Aircraft, measured in Length can be negative.

What unit is used to measure Optimum Range of Aircraft?

Optimum 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 Optimum Range of Aircraft can be measured.

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