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NF-6风洞马赫数控制系统研制
引用本文:惠增宏,何明一,竹朝霞.NF-6风洞马赫数控制系统研制[J].实验流体力学,2005,19(1):61-65.
作者姓名:惠增宏  何明一  竹朝霞
作者单位:西北工业大学,陕西,西安,710072
摘    要:NF-6风洞是我国唯一一座增压连续式跨声速翼型风洞,为了提高实验雷诺数,在设计上还具有喷氮降温的功能。笔者介绍了NF-6风洞马赫数控制系统的组成、特点及运行方式,对转速控制子系统、压缩机静叶角控制子系统、二喉道栅指控制子系统等进行了较为详细的介绍。

关 键 词:跨声速风洞  马赫数  转速控制  静叶角  二喉道栅指  NF-6
文章编号:1672-9897(2005)01-0061-05
修稿时间:2004年4月12日

Research on the Mach number control system in NF-6 wind tunnel
HUI Zeng-hong,HE Ming-yi,ZHU Zhao-xia.Research on the Mach number control system in NF-6 wind tunnel[J].Experiments and Measur in Fluid Mechanics,2005,19(1):61-65.
Authors:HUI Zeng-hong  HE Ming-yi  ZHU Zhao-xia
Abstract:NF-6 wind tunnel is a pressurized continuous two-dimensional transonic wind tunnel, which is the only one in China. In this paper, the Mach number control system in NF-6 wind tunnel is introduced, especially in detail for the compressor rotary speed control sub-system, the compressor stator vane control sub-system and the second throat control sub-system.
Keywords:transonic wind tunnel  Mach number  compressor rotary speed control  compressor stator vane control  second throat control
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