Calculations of shock-wave flow structure in axisymmetric channel with near-wall ethylene burning with throttle air jet

V. P. Zamuraev, A. P. Kalinina, D. V. Fedorova, D. S. Popova

Результат исследования: Научные публикации в периодических изданияхстатья по материалам конференции

Аннотация

The CFD modelling of the ramjet start with low losses of the stagnation pressure was carried out. The basic feature of this start technology was the jet of compressed air creating effect of a throttle which aids in preliminary decelerating of the flow up to transonic velocities. The comparison with experiment was performed for the hydrogen burning. We studied the axial and near-wall supply of gas fuel. The physical mechanisms stimulating stable presence of transonic mode in the part with constant section were investigated within the frameworks URANS approach. It was shown that fuel supply blockage is a way to control near-wall supplying of gaseous fuel at considerably low pressure falls. And blocking the ignition processes is a way to control the axial supply at quite high pressure falls.

Язык оригиналаанглийский
Номер статьи012066
ЖурналJournal of Physics: Conference Series
Том1369
Номер выпуска1
DOI
СостояниеОпубликовано - 26 ноя 2019
Событие5th International Workshop on Heat/Mass Transfer Advances for Energy Conservation and Pollution Control, IWHT 2019 - Novosibirsk, Российская Федерация
Продолжительность: 13 авг 201916 авг 2019

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