Regularities of the interaction of hydrogen jets during combustion in a supersonic high-temperature flow

被引：0

作者：

V. A. Zabaykin

A. A. Smogolev

机构：

[1] Russian Academy of Sciences,Institute of Theoretical and Applied Mechanics, Siberian Division

来源：

Russian Journal of Physical Chemistry B | 2007年 / 1卷

关键词：

Mach Disk; Nozzle Pressure Ratio; Shock Train; Axial Injector; Fuel Feed;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

The efficiency of combustion in a supersonic high-temperature flow at spread and local hydrogen feed is considered. Similarities and distinctions of combustion in open and confined space were examined with consideration given to the effect of gasdynamic structures typical of supersonic air jets.

引用

页码：245 / 249

页数：4

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