Hydrogen combustion under conditions of a high-temperature supersonic flow

被引:4
|
作者
Zabaykin, V. A. [1 ]
机构
[1] Russian Acad Sci, Siberian Branch, Khristianovich Inst Theoret & Appl Mech, Novosibirsk 630090, Russia
关键词
HIGH-ENTHALPY; AIR-FLOW; EFFICIENCY; INJECTION;
D O I
10.1134/S0018151X1704023X
中图分类号
O59 [应用物理学];
学科分类号
摘要
Some results of studying the combustion of hydrogen in a high-velocity air flow at stagnation temperatures below 3000 K are given. Flame shape and combustion zone length change at temperatures above 2000-2200 K due to deterioration in the fuel-oxidizer mixing process. It has been shown that dissociation processes have an effect on the process of hydrogen combustion at a high temperature. In experiments, they can be detected by a change in the intensity of radiation from the intermediate DDe* radical.
引用
收藏
页码:567 / 572
页数:6
相关论文
共 50 条