Effect of high temperatures on the combustion of hydrogen in a supersonic flow

被引：0

作者：

V. A. Zabaikin

A. A. Smogolev

机构：

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

来源：

Russian Journal of Physical Chemistry B | 2008年 / 2卷

关键词：

Mach Number; Emission Intensity; Combustion Chamber; Supersonic Flow; Stagnation Temperature;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

The results of experiments on studying the effect of temperature on the character of burnout and emission characteristics of a hydrogen flow symmetrically injected into a supersonic air flow are presented. The combustion of hydrogen in the supersonic flow at 1500–3000 K is demonstrated to be affected by dissociation and recombination. This manifests itself through an increase in the OH emission intensity by 40% upon 1.5–2.0-fold temperature rise starting from 1500 K.

引用

页码：775 / 778

页数：3

共 50 条

[1] Effect of High Temperatures on the Combustion of Hydrogen in a Supersonic Flow
Zabaikin, V. A.
Smogolev, A. A.
RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B, 2008, 2 (05) : 775 - 778
[2] Hydrogen combustion under conditions of a high-temperature supersonic flow
V. A. Zabaykin
High Temperature, 2017, 55 : 567 - 572
[3] Hydrogen combustion under conditions of a high-temperature supersonic flow
Zabaykin, V. A.
HIGH TEMPERATURE, 2017, 55 (04) : 567 - 572
[4] Diffusion combustion of a system of plane supersonic hydrogen jets in a supersonic flow
Zhapbasbaev, UK
Makashev, EP
COMBUSTION EXPLOSION AND SHOCK WAVES, 2003, 39 (04) : 415 - 422
[5] Ignition and combustion of hydrogen in a channel with high supersonic flow velocities at the channel entrance
Vinogradov, V. A.
Goldfeld, M. A.
Starov, A. V.
COMBUSTION EXPLOSION AND SHOCK WAVES, 2013, 49 (04) : 383 - 391
[6] Diffusion Combustion of a System of Plane Supersonic Hydrogen Jets in a Supersonic Flow
U. K. Zhapbasbaev
E. P. Makashev
Combustion, Explosion and Shock Waves, 2003, 39 : 415 - 422
[7] Ignition and combustion of hydrogen in a channel with high supersonic flow velocities at the channel entrance
V. A. Vinogradov
M. A. Goldfeld
A. V. Starov
Combustion, Explosion, and Shock Waves, 2013, 49 : 383 - 391
[8] NONEQUILIBRIUM MODEL FOR HYDROGEN COMBUSTION IN SUPERSONIC-FLOW
CORREA, SM
MANI, R
JOURNAL OF PROPULSION AND POWER, 1989, 5 (05) : 523 - 528
[9] Hydrogen combustion in an axisymmetric duct with a supersonic air flow
Zabaykin, V. A.
Smogelev, A. A.
COMBUSTION EXPLOSION AND SHOCK WAVES, 2007, 43 (03) : 247 - 252
[10] Hydrogen combustion in an axisymmetric duct with a supersonic air flow
V. A. Zabaykin
A. A. Smogolev
Combustion, Explosion, and Shock Waves, 2007, 43 : 247 - 252

← 1 2 3 4 5 →