CONTROL OF THE SUPERSONIC FLOW STRUCTURE DURING ETHYLENE COMBUSTION WITH THE USE OF GAS-DYNAMIC PULSES

被引：0

作者：

V. P. Zamuraev

A. P. Kalinina

机构：

[1] Khristianovich Institute of Theoretical and Applied Mechanics,

[2] Siberian Branch,undefined

[3] Russian Academy of Sciences,undefined

来源：

Journal of Applied Mechanics and Technical Physics | 2021年 / 62卷

关键词：

ethylene combustion; axial injector; supersonic flow; throttling jet; transonic flow;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：1 / 10

页数：9

共 29 条

[1] CONTROL OF THE SUPERSONIC FLOW STRUCTURE DURING ETHYLENE COMBUSTION WITH THE USE OF GAS-DYNAMIC PULSES
Zamuraev, V. P.
Kalinina, A. P.
JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2021, 62 (01) : 1 - 10
[2] Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers
Zamuraev, V. P.
Kalinina, A. P.
COMBUSTION EXPLOSION AND SHOCK WAVES, 2022, 58 (04) : 450 - 456
[3] Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers
V. P. Zamuraev
A. P. Kalinina
Combustion, Explosion, and Shock Waves, 2022, 58 : 450 - 456
[4] Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow
V. P. Zamuraev
A. P. Kalinina
Thermophysics and Aeromechanics, 2018, 25 : 149 - 152
[5] Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow
Zamuraev, V. P.
Kalinina, A. P.
THERMOPHYSICS AND AEROMECHANICS, 2018, 25 (01) : 149 - 152
[6] Combustion of Kerosene in a Supersonic Flow at Mach Number M = 1.7 Under the Action of Gas-Dynamical Pulses
V. P. Zamuraev
A. P. Kalinina
Journal of Engineering Physics and Thermophysics, 2023, 96 : 906 - 912
[7] Combustion of Kerosene in a Supersonic Flow at Mach Number M = 1.7 Under the Action of Gas-Dynamical Pulses
Zamuraev, V. P.
Kalinina, A. P.
JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2023, 96 (4) : 906 - 912
[8] Gas-dynamic problems in off-design operation of supersonic inlets (review)
V. I. Zvegintsev
Thermophysics and Aeromechanics, 2017, 24 : 807 - 834
[9] Gas-dynamic problems in off-design operation of supersonic inlets (review)
Zvegintsev, V. I.
THERMOPHYSICS AND AEROMECHANICS, 2017, 24 (06) : 807 - 834
[10] Numerical simulation of the unsteady propagation of combustion in a duct with a supersonic viscous gas flow
V. V. Vlasenko
Russian Journal of Physical Chemistry B, 2011, 5 : 800 - 812

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