...
首页> 外文期刊>Chinese journal of aeronautics >Experimental and Analytical Investigation on Aerodynamic Characteristics of Helicopter Scissors Tail Rotor
【24h】

Experimental and Analytical Investigation on Aerodynamic Characteristics of Helicopter Scissors Tail Rotor

机译:直升机剪刀式尾桨气动特性的实验和分析研究

获取原文
获取原文并翻译 | 示例
           

摘要

An experimental and analytical investigation on the aerodynamic characteristics of a heli- copter scissors tail rotor has been made. The experiments are carried out on a model rotor rig and the variations of the rotor thrust and torque with scissors angles are investigated. The effects of two dif- ferent configurations, i.e., Configuration L in which the lower blade is in front of the upper blade and configuration U in which the upper blade is in front of the lower blade, on rotor performance are compared.
机译:对直升机剪刀式尾桨的空气动力学特性进行了实验和分析研究。实验是在模型转子装置上进行的,研究了转子推力和转矩随剪刀角的变化。比较了两种不同的配置,即配置L(其中下部叶片位于上部叶片之前)和配置U(其中上部叶片位于下部叶片之前)对转子性能的影响。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号