Weight of Aircraft at End of Loiter Phase in Aircraft Design Formulas

Weight of Aircraft at End of Loiter Phase is considered for the Preliminary Endurance Calculation. For the calculation of preliminary endurance, the loiter phase is considered. And is denoted by W_L,end. Weight of Aircraft at End of Loiter Phase is usually measured using the Kilogram for Weight. Note that the value of Weight of Aircraft at End of Loiter Phase is always positive. Typically, the value of Weight of Aircraft at End of Loiter Phase is greater than 0.

Aircraft Design formulas that make use of Weight of Aircraft at End of Loiter Phase

fxPreliminary Endurance for Prop-Driven AircraftGo

fxVelocity at Maximum Endurance given Preliminary Endurance for Prop-Driven AircraftGo

FAQ

What is the Weight of Aircraft at End of Loiter Phase?

Weight of Aircraft at End of Loiter Phase is considered for the Preliminary Endurance Calculation. For the calculation of preliminary endurance, the loiter phase is considered. Weight of Aircraft at End of Loiter Phase is usually measured using the Kilogram for Weight. Note that the value of Weight of Aircraft at End of Loiter Phase is always positive. Typically, the value of Weight of Aircraft at End of Loiter Phase is greater than 0.

Can the Weight of Aircraft at End of Loiter Phase be negative?

No, the Weight of Aircraft at End of Loiter Phase, measured in Weight cannot be negative.

What unit is used to measure Weight of Aircraft at End of Loiter Phase?

Weight of Aircraft at End of Loiter Phase is usually measured using the Kilogram[kg] for Weight. Gram[kg], Milligram[kg], Ton (Metric)[kg] are the few other units in which Weight of Aircraft at End of Loiter Phase can be measured.

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