Free piston shock tunnels: developments and capabilities
SL Gai - Progress in Aerospace Sciences, 1992 - Elsevier
The free piston shock tunnel has shown itself to be uniquely capable of adequately
simulating real gas effects and has been successfully operating in Australia for more than …
simulating real gas effects and has been successfully operating in Australia for more than …
[HTML][HTML] 自由活塞高焓脉冲风洞发展历程及试验能力综述
陈星， 谌君谋， 毕志献， 马汉东 - 实验流体力学, 2019 - pubs.cstam.org.cn
自由活塞高焓脉冲风洞是研究高温气体效应主要的地面模拟设备之一, 具备模拟超高速流动的
能力, 主要分为自由活塞驱动的高焓激波风洞和高焓膨胀管风洞. 经过数十年的发展 …
能力, 主要分为自由活塞驱动的高焓激波风洞和高焓膨胀管风洞. 经过数十年的发展 …
Measurement techniques in high-enthalpy hypersonic facilities
JM Simmons - Experimental thermal and fluid science, 1995 - Elsevier
Interest in hypersonic aerodynamic braking and aerospace planes has led to the
development of new high-enthalpy hypersonic test facilities. This paper describes available …
development of new high-enthalpy hypersonic test facilities. This paper describes available …
[HTML][HTML] 高超声速喷管设计理论与方法
汪运鹏， 姜宗林 - 力学进展, 2021 - lxjz.cstam.org.cn
在高超声速飞行技术领域, 特别是涉及到高焓气体流动的研究, 高超声速风洞试验仍然是目前最
可靠的研究手段. 风洞流场的品质是高超声速风洞研发最重要的一项性能指标 …
可靠的研究手段. 风洞流场的品质是高超声速风洞研发最重要的一项性能指标 …
Flow characterization of a hypersonic expansion tube facility for supersonic combustion studies
YM Abul-Huda, M Gamba - Journal of Propulsion and Power, 2017 - arc.aiaa.org
A hypersonic expansion tube facility was designed and constructed to primarily study
supersonic combustion phenomena. This paper provides an overview of the range of …
supersonic combustion phenomena. This paper provides an overview of the range of …
[图书][B] Scanned wavelength-modulation absorption spectroscopy with application to hypersonic impulse flow facilities
CL Strand - 2014 - search.proquest.com
The work presented herein describes several advances in the evolution of combustion
diagnostics based upon the technique of tunable diode laser absorption spectroscopy …
diagnostics based upon the technique of tunable diode laser absorption spectroscopy …
[HTML][HTML] 自由活塞激波风洞压缩管非等熵流动分析
易翔宇， 陈星， 毕志献， 陈农， 纪锋， 谌君谋， 姚大鹏 - 气体物理, 2021 - xml-data.org
在自由活塞驱动的高超声速地面试验设备中, 自由活塞压缩器的运行状态对于试验气流状态参数
, 试验时间及设备安全性起到决定性的作用. 研究基于FD-21 自由活塞激波风洞结构参数 …
, 试验时间及设备安全性起到决定性的作用. 研究基于FD-21 自由活塞激波风洞结构参数 …
大尺寸自由活塞激波风洞重活塞软着陆关键技术
谌君谋， 陈星， 易翔宇， 孙日明， 纪锋… - 空气动力学 …, 2023 - kqdlxxb.xml-journal.net
高焓激波风洞的驱动技术决定了风洞总焓和总压试验能力. 重活塞压缩加热技术具有驱动性能强
和运行灵活性高等特点, 是高焓激波风洞关键驱动技术. 针对重活塞发射效能 …
和运行灵活性高等特点, 是高焓激波风洞关键驱动技术. 针对重活塞发射效能 …
[图书][B] Hot experimental technique: a new requirement of aerothermodynamics
EH Hirschel - 1993 - Springer
The flow past hypersonic vehicles causes large heat loads on the vehicle surfaces. It is
shown that the heat loads and the flow properties are strongly coupled, if radiation cooling is …
shown that the heat loads and the flow properties are strongly coupled, if radiation cooling is …
Characteristics of the AT-303 hypersonic wind tunnel. Part 1. Velocity fields
AM Kharitonov, VI Zvegintsev, LG Vasenev… - Thermophysics and …, 2006 - Springer
The structure and principle of operation of a new wind tunnel AT-303 with adiabatic
compression are described. Results of systematic investigations are presented in terms of …
compression are described. Results of systematic investigations are presented in terms of …