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Unique Range Performance Properties of Electric Aircraft

机译：电动飞机的独特射程性能

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Aircraft equipped with an electric propulsion system feature unique range performance properties. Range performance topics dealt with include basic properties in terms of maximum-range cruise in zero wind cruise as well as the effects of head- and tailwinds. It is shown that range performance properties of electric aircraft differ considerably from those of comparable vehicles with an air-breathing propulsion system. It turns out that electric aircraft can show significant performance advantages. Analytical solutions of the range performance problems are derived so that results of generally valid nature are obtained. This is supplemented by computational results used as exemplary cases in order to provide a quantitative insight.
机译：配备电动推进系统的飞机具有独特的航程性能。范围性能主题涉及的基本属性包括零风速巡航的最大范围巡航以及顺风和逆风的影响。结果表明，电动飞机的航程性能特性与具有空气呼吸推进系统的同类车辆相比有很大差异。事实证明，电动飞机可以显示出显着的性能优势。得出了测距性能问题的解析解，从而获得了总体上有效的结果。此外，还提供了用作示例性案例的计算结果，以提供定量的见解。

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