高超声速机体/推进一体化试验设备概述

An overview of hypersonic aero-propulsion integration test facilities

回顾了高超声速推进地面设备及任务的发展历程,明确了设备分类,简述了直连式超声速燃烧试验台、燃烧加热高超声速高温风洞、电弧加热超声速燃烧试验台、高超声速高焓激波试验台、脉冲燃烧风洞等试验设备的原理、主要结构和基本参数。通过对不同设备特点的分析,指出脉冲燃烧风洞是开展高超声速机体/推进一体化试验的理想设备。

The history of hypersonic propulsion facilities and tasks are briefly reviewed in this paper,the operating principle,main structures and basic parameters of these reclassified facilities are also surveyed,including direct-connect supersonic combustion test facility,combustion-heated high temperature tunnel,arc-heated scramjet test facility,high enthalpy shockwave facility and combustion-heated impulse tunnel.After an analysis of the characteristics of different facilities,it is pointed out that the combustion-heated impulse tunnel is the ideal facility for aero-propulsion integration test.