This manuscript describes the wide variety of optical measurement techniques for
characterizing the flow in hypersonic wind tunnels. The introduction briefly describes …

This work examined combustion modes in a fundamental, axisymmetric, supersonic
combustor at flight equivalent Mach numbers ranging from 7.5 to 9.0. Ethylene was injected …

The design and testing of a cavity flameholder in a Mach 8 rectangular-to-elliptical shape-
transitioning scramjet is presented. The experimental results presented are from the shock …

The characteristics of a hydrogen jet flame in a one-sided divergent scramjet combustor are
investigated using both experiments and large-eddy simulations. Optical observations …

Hypersonic airbreathing engines rely on scramjet combustion processes, which involve high-
speed, compressible, and highly turbulent reacting flows. The combustion environment and …

This work describes the characterization of flame stabilization mechanisms present in a
recirculation-stabilized ethylene-air flame in supersonic co-flow. OH-PLIF measurements are …

In recent years, significant research attention has focused on scramjet bench-testing using
optical measurement techniques to obtain significant experimental data. The work aims to …

Hydroxyl tagging velocimetry (HTV) technology is crucial in the velocimetry diagnosis of
combustion flow fields. However, obtaining accurate HTV information in practical …

2 ENVIRONMENT: TRACE GAS MONITORING of the spectroscopy underlying the
respective technique and the use of sophisticated equipment in order to obtain meaningful …

为满足超燃冲压发动机燃烧诊断尤其是燃烧空间结构可视化的迫切需求, 亟需实现超声速火焰
三维测量. 三维激光诱导荧光(3DLIF) 技术作为一种立体测量技术具有超声速火焰三维测量的 …