Abstract
The influence of shock patterns, rearward facing steps and multistep fuel injection on mixing and combustion processes in supersonic hydrogen/air flames was investigated by means of non-intrusive optical measurement techniques. The tests showed that rearward facing steps and multistep fuel injection generate vortices in the mixing jet which enhanced the mixing and combustion processes.
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Gabler, W., Haibel, M., Mayinger, F. (1995). Mixing Process in Reacting and Non-Reacting Supersonic Flows. In: Benzi, R. (eds) Advances in Turbulence V. Fluid Mechanics and Its Applications, vol 24. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-0457-9_28
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DOI: https://doi.org/10.1007/978-94-011-0457-9_28
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