节点文献

大型连续式跨声速风洞总体方案与关键技术研究

Characteristics and key technology analysis of large continuous transonic wind tunnel

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 陈振华刘宗政陈吉明郭守春闫喜强裴海涛

【Author】 CHEN Zhenhua;LIU Zongzheng;CHEN Jiming;GUO Shouchun;YAN Xiqiang;PEI Haitao;Facility Design and Instrumentation Institute,China Aerodynamics Research and Development Center;

【通讯作者】 陈吉明;

【机构】 中国空气动力研究与发展中心设备设计与测试技术研究所

【摘要】 大型连续式跨声速风洞具备飞行器外形精确模拟、气动弹性评估和机体/推进一体化设计等试验能力,试验段尺寸大、指标要求高、系统规模大、运行功能多。围绕大型连续式跨声速风洞的特点,简要介绍了大型连续式跨声速风洞总体设计方案,重点介绍了世界一流流场品质实现、大型轴流压缩机及其驱动系统研制等关键技术的初步研究成果。

【Abstract】 The large scale continuous transonic wind tunnel has several main features, such as the large-size test section, high wind tunnel performance specifics, large scale wind tunnel system,multi-function wind tunnel operation. It has the test capabilities of accurate simulation of the aircraft shape, aero-elastic evaluation and integrated body/propulsion design. This paper briefly introduces the overall design of the large continuous transonic wind tunnel, and special focus is put on the preliminary research results of key technologies such as the realization of world-class flow quality and the development of the large axial compressor and its driving system.

  • 【文献出处】 实验流体力学 ,Journal of Experiments in Fluid Mechanics , 编辑部邮箱 ,2022年01期
  • 【分类号】V211.74
  • 【被引频次】1
  • 【下载频次】122
节点文献中: 

本文链接的文献网络图示:

本文的引文网络