[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 …
Simultaneous measurement of aerodynamic and heat transfer data for large angle blunt cones in hypersonic shock tunnel
Aerodynamic forces and fore-body convective surface heat transfer rates over a 60° apex-
angle blunt cone have been simultaneously measured at a nominal Mach number of 5.75 in …
angle blunt cone have been simultaneously measured at a nominal Mach number of 5.75 in …
A new single stage driver for the X2 expansion tube
The X2 expansion tube is one of three expansion tubes located at the University of
Queensland. Installation of the facility was completed in the middle of 1995 and …
Queensland. Installation of the facility was completed in the middle of 1995 and …
Post-shock thermochemistry in hypervelocity CO2 and air flow
M Sharma - 2010 - ideals.illinois.edu
This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in
anticipation of the upcoming Mars Science Laboratory (MSL) and future missions to the red …
anticipation of the upcoming Mars Science Laboratory (MSL) and future missions to the red …
Sonic line location in reacting flows
R Morgan, M Abdel-Jawad, D Mee - 40th AIAA Aerospace Sciences …, 2002 - arc.aiaa.org
Superorbital re-entry vehicles involve blunt configurations, and are designed to operate near
to the limits of stability in order to produce the best possible aerodynamic characteristics …
to the limits of stability in order to produce the best possible aerodynamic characteristics …