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Lift offset: an analytical insight

机译:提升偏移量:分析见解

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摘要

Purpose - This paper aims to present an analytical insight into the effect known as lift offset. This effect may be of advantage in terms of power consumption when configurations that consists of two main rotors (coaxial, tandem, etc.) are operated at high speed forward flight. Fundamentally, each of the main rotors is producing a roll moment in opposite direction that is overall canceled to allow trim. The first-order phenomena of lift offset are therefore related to the load distribution over each rotor and may be analyzed independently of the interaction between the rotors.
机译:目的-本文旨在对所谓的升程偏移量的影响进行分析。当由两个主旋翼(同轴,串联等)组成的配置在高速向前飞行时,这种效果在功耗方面可能是有利的。根本上,每个主旋翼都会产生相反方向的侧倾力矩,该力矩会被完全抵消以实现微调。因此,升程偏移的一阶现象与每个转子上的负载分布有关,并且可以独立于转子之间的相互作用而进行分析。

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