Progress in shock wave/boundary layer interactions
DV Gaitonde - Progress in Aerospace Sciences, 2015 - Elsevier
Recent advances in shock wave boundary layer interaction research are reviewed in four
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …
Materials design for hypersonics
Hypersonic vehicles must withstand extreme conditions during flights that exceed five times
the speed of sound. These systems have the potential to facilitate rapid access to space …
the speed of sound. These systems have the potential to facilitate rapid access to space …
Quiet tunnel measurements of HIFiRE-5 boundary-layer transition
TJ Juliano, MP Borg, SP Schneider - AIAA Journal, 2015 - arc.aiaa.org
The Hypersonic International Flight Research Experimentation (HIFiRE) program is a
hypersonic flight test program executed by the Air Force Research Laboratory and …
hypersonic flight test program executed by the Air Force Research Laboratory and …
激波风洞超燃冲压发动机推力测量技术研究
赵荣娟， 刘施然， 周正， 吴里银， 吕治国 - 实验流体力学, 2022 - syltlx.com
为满足高马赫数超燃冲压发动机研制的需求, 在激波风洞中开展了超燃冲压发动机推力测量技术
研究工作, 采用压电式推力测量天平测量了超燃冲压发动机模型上的推力. 根据试验模型的受力 …
研究工作, 采用压电式推力测量天平测量了超燃冲压发动机模型上的推力. 根据试验模型的受力 …
Analysis of second-mode amplitudes on sharp cones in hypersonic wind tunnels
EC Marineau, G Grossir, A Wagner… - Journal of Spacecraft …, 2019 - arc.aiaa.org
This research effort coordinated by the NATO Science and Technology Organization Applied
Vehicle Technology 240 specialists' group compiles and analyzes second-mode amplitudes …
Vehicle Technology 240 specialists' group compiles and analyzes second-mode amplitudes …
[HTML][HTML] 高焓激波风洞试验技术综述
谌君谋， 陈星， 毕志献， 马汉东 - 空气动力学学报, 2018 - html.rhhz.net
高焓激波风洞是研究高温真实气体效应主要的地面模拟设备, 基于高焓激波风洞发展的试验技术
主要包括驱动技术, 流场检测技术和测试技术. 决定试验段所能达到的总焓和总压水平的驱动 …
主要包括驱动技术, 流场检测技术和测试技术. 决定试验段所能达到的总焓和总压水平的驱动 …
HIFiRE-5b heat flux and boundary-layer transition
Hypersonic International Flight Research Experimentation (HIFiRE)-5 is a hypersonic flight-
test experiment designed to investigate the aerothermodynamics of a three-dimensional …
test experiment designed to investigate the aerothermodynamics of a three-dimensional …
HIFiRE-5 flight test results
TJ Juliano, D Adamczak, RL Kimmel - Journal of Spacecraft and …, 2015 - arc.aiaa.org
The Hypersonic International Flight Research Experimentation (HIFiRE-5) is a hypersonic
flight test vehicle designed to investigate the aerothermodynamics of a three-dimensional …
flight test vehicle designed to investigate the aerothermodynamics of a three-dimensional …
Streak instabilities on HIFiRE-5 elliptic cone
MM Choudhari, F Li, P Paredes - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
The Hypersonic International Flight Research and Experimentation (HIFiRE) 5 flight
experiment by the Air Force Research Laboratories and Australian Defense Science and …
experiment by the Air Force Research Laboratories and Australian Defense Science and …
Assessment of new pressure-corrected design method for hypersonic internal waverider intake
O Musa, G Huang, Z Yu - Acta Astronautica, 2022 - Elsevier
The osculating axisymmetric flows concept is an extension of the concept of the osculating
cones for designing waveriders which is also utilized to design the three-dimensional …
cones for designing waveriders which is also utilized to design the three-dimensional …