Special features of the combustion process in a channel with a supersonic velocity at the entrance

被引：0
|
作者：
V. K. Baev
P. K. Tret’yakov
V. V. Shumskii
机构：
[1] Russian Academy of Sciences,Institute of Theoretical and Applied Mechanics Siberian Division
来源：
Combustion, Explosion and Shock Waves | 1999年 / 35卷
关键词：
Mach Number; Supersonic Flow; Oscillatory Process; Hydrogen Flow Rate; Supersonic Velocity;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Results of combustion studies in channels are presented. These researches deal with anomalous phenomena in steady turbulent flows: unsteady heat transfer, two-layer flow, oscillations of a gas column of different intensity and frequency. Under certain conditions, these phenomena lead to substantial redistributions of enthalphy and stagnation pressure at the exit of the combustion chamber, which significantly affects the integral characteristics of the combustor.
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页码：370 / 378
页数：8
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