Measurements of T5 shock tunnel freestream temperature, velocity, and composition

PM Finch, JJ Girard, T Schwartz, CL Strand… - AIAA Journal, 2023 - arc.aiaa.org
We report on measurements of rotational and vibrational temperature, velocity, and
concentrations of nitric oxide (NO) in freestream flows at the T5 reflected shock tunnel at …

Shock-layer measurements in T5 shock tunnel hypersonic flows around a cylinder model

PM Finch, JJ Girard, T Schwartz, CL Strand… - AIAA Journal, 2024 - arc.aiaa.org
We report on near-body measurements of temperature and nitric oxide (NO) concentration in
the hypersonic flows around a cylindrical test article in the Caltech T5 reflected shock tunnel …

Non-intrusive measurement techniques for flow characterization of hypersonic wind tunnels

PM Danehy, J Weisberger, C Johansen, D Reese… - 2018 - ntrs.nasa.gov
This manuscript describes the wide variety of optical measurement techniques for
characterizing the flow in hypersonic wind tunnels. The introduction briefly describes …

Characterization of the T5 reflected shock tunnel freestream temperature, velocity, and composition using laser absorption spectroscopy

J Girard, PM Finch, T Schwartz, W Yu… - AIAA Propulsion and …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3525. vid We report on
measurements of rotational and vibrational temperature, velocity, and concentrations of nitric …

Collisional radiative modeling of electronically excited states in a hypersonic flow

IT Karpuzcu, MP Jouffray, DA Levin - Journal of Thermophysics and …, 2022 - arc.aiaa.org
The hypersonic, nonequilibrium thermochemistry flow over a cylinder was modeled to study
nitric oxide (NO) ultraviolet (UV) emissions. The main focus of this work is to model the …

Vacuum ultraviolet spectral measurements for superorbital earth entry in X2 expansion tube

UA Sheikh, RG Morgan, TJ McIntyre - Aiaa Journal, 2015 - arc.aiaa.org
Experiments were conducted using the X2 expansion tube at two conditions representative
of flight velocities of 10.0 and 12.2 km/s for a vehicle entry into Earth's atmosphere …

VUV to IR Emission Spectroscopy and Interferometry Diagnostics for the European Shock Tube for High-Enthalpy Research

R Grosso Ferreira, BB Carvalho, LL Alves, B Gonçalves… - Sensors, 2023 - mdpi.com
The European Shock Tube for High-Enthalpy Research is a new state-of-the-art facility,
tailored for the reproduction of spacecraft planetary entries in support of future European …

[PDF][PDF] 可调谐半导体激光吸收光谱技术在高超声速风洞中的应用研究进展

方洪鑫, 支冬, 吴学成, 李云飞, 常雨, 陈卫… - Laser & …, 2024 - researching.cn
摘要高超声速风洞在航空航天领域占据着不可替代的作用. 可调谐半导体激光吸收光谱技术(
TDLAS) 是一种具备非接触, 灵敏度高, 多参数测量, 结构简单, 价格低廉和高时空分辨等优点的 …

Spectral measurements of hypervelocity flow in an expansion tunnel

CK Yuan, K Zhou, YF Liu, ZM Hu, ZL Jiang - Acta Mechanica Sinica, 2019 - Springer
Atmospheric reentry vehicles and planetary probes fly through the atmosphere at
hypervelocity speed. At such speed, there is a significant proportion of heat load to the …

氮气辐射强度的激波管测量与验证

吕俊明, 李飞, 林鑫, 程晓丽, 余西龙, 俞继军 - 实验流体力学, 2019 - syltlx.com
超高速飞行器的热防护设计必须考虑激波层内高温气体发射与吸收的辐射能量,
需要有效的辐射加热评估手段. 相应飞行条件下的光谱辐射强度地面实验测量是验证数值模型和 …