Preliminary Endurance of Aircraft in Aircraft Design Formulas

Preliminary Endurance of Aircraft is the maximum length of time that an aircraft can spend in cruising flight. And is denoted by P_E. Preliminary Endurance of Aircraft is usually measured using the Second for Time. Note that the value of Preliminary Endurance of Aircraft is always positive.

Formulas to find Preliminary Endurance of Aircraft in Aircraft Design

fxPreliminary Endurance for Jet AircraftGo

List of variables in Aircraft Design formulas

fx Maximum Lift-to-Drag Ratio of Aircraft Go

fx Weight of Aircraft at Beginning of Cruise Phase Go

fx Weight of Aircraft at End of Cruise Phase Go

fx Power Specific Fuel Consumption Go

FAQ

What is the Preliminary Endurance of Aircraft?

Preliminary Endurance of Aircraft is the maximum length of time that an aircraft can spend in cruising flight. Preliminary Endurance of Aircraft is usually measured using the Second for Time. Note that the value of Preliminary Endurance of Aircraft is always positive.

Can the Preliminary Endurance of Aircraft be negative?

No, the Preliminary Endurance of Aircraft, measured in Time cannot be negative.

What unit is used to measure Preliminary Endurance of Aircraft?

Preliminary Endurance of Aircraft is usually measured using the Second[s] for Time. Millisecond[s], Microsecond[s], Nanosecond[s] are the few other units in which Preliminary Endurance of Aircraft can be measured.

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