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直升机高原悬停地面效应的研究

田磊 刘国强 李亮明

航空科学技术2016,Vol.27Issue(7):39-43,5.
航空科学技术2016,Vol.27Issue(7):39-43,5.

直升机高原悬停地面效应的研究

Helicopter Ground Effect on Plateau Based on Hover

田磊 1刘国强 1李亮明1

作者信息

  • 1. 中国飞行试验研究院,陕西 西安 710089
  • 折叠

摘要

Abstract

Research on the helicopter ground effect at different altitude based on the result of helicopter flight test on plateau. Through the analysis of theCt~Mk curve, obtained by the flight test result for helicopter hovering with the different altitudes, weights and height above the ground, proposed the helicopter ground effect function model suitable for high altitude flight test. Based on this model, the numerical result was given the influence of the altitude of the helicopter ground effect. It is important for the follow-up helicopter plateau flight test.

关键词

直升机/地面效应/飞行试验/悬停/高原

Key words

helicopter/ground effect/flight test/hover/plateau

分类

航空航天

引用本文复制引用

田磊,刘国强,李亮明..直升机高原悬停地面效应的研究[J].航空科学技术,2016,27(7):39-43,5.

航空科学技术

1007-5453

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