CONTROL OF THE SELF-OSCILLATION OF AMPLITUDE OF VIBRATION COMBUSTION IN A LIQUID-PROPELLANT ROCKET ENGINE BY SOLVING THE SYSTEM OF EQUATIONS THAT DESCRIBE THIS REGIME OF COMBUSTION

被引：0

作者：

Gotsulenko, V. V. ^{[1
]}

机构：

[1] Zheltye Vody Inst Enterprise Strategy, 38 Gagarin Str, UA-52201 Zheltye Vody, Ukraine

来源：

JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS | 2010年 / 83卷 / 03期

关键词：

degenerate system; limiting cycle; control of the amplitude; vibration combustion;

D O I：

10.1007/s10891-010-0373-8

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

Periodic solutions of the degenerate system of equations of nonstationary motion of a medium in a liquid-pro-pellant rocket engine were obtained, with the aid of which the possibility of lowering the amplitude of the longitudinal self-oscillations of vibration combustion or their complete removal has been substantiated.

引用

页码：525 / 531

页数：7

共 16 条

[1] SELF-OSCILLATIONS OF AN UNSTABLE FUEL COMBUSTION IN THE COMBUSTION CHAMBER OF A LIQUID-PROPELLANT ROCKET ENGINE
Gotsulenko, V. V.
Gotsulenko, V. N.
JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2013, 86 (01) : 160 - 165
[2] CONCERNING THE PROBLEM OF DYNAMIC DAMPING OF THE VIBRATION COMBUSTION SELF-OSCILLATIONS IN A LIQUID-PROPELLANT ROCKET ENGINE
Basok, B. I.
Gotsulenko, V. V.
Gotsulenko, V. N.
JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2012, 85 (06) : 1346 - 1351
[3] Concerning the problem of dynamic damping of the vibration combustion self-oscillations in a liquid-propellant rocket engine
B. I. Basok
V. V. Gotsulenko
V. N. Gotsulenko
Journal of Engineering Physics and Thermophysics, 2012, 85 (6) : 1346 - 1351
[4] MECHANISM OF FLAME AUTOSTABILIZATION IN COMBUSTION CHAMBER OF A LIQUID-PROPELLANT ROCKET ENGINE
BELYI, VV
DOKLADY AKADEMII NAUK SSSR, 1971, 201 (06): : 1326 - &
[5] Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine
Zarubin V.S.
Zimin V.N.
Kuvyrkin G.N.
Russian Aeronautics, 2018, 61 (03): : 425 - 433
[6] Method for Predicting the Stability Limit to Acoustic Oscillations in Liquid-Propellant Rocket Engine Combustion Chambers Based on Combustion Noise
V. I. Biryukov
V. N. Ivanov
R. A. Tsarapkin
Combustion, Explosion, and Shock Waves, 2021, 57 : 74 - 82
[7] Off-Design Combustion in Liquid-Propellant Rocket Engine with High-Frequency Instability
Kanda, Takeshi
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2019, 62 (06) : 331 - 333
[8] ON THE CYCLIC DEFORMATION OF THE SHELL OF THE COMBUSTION CHAMBER OF A MULTIPLE-ACTION LIQUID-PROPELLANT ROCKET ENGINE
Zarubin, V. S.
Zimin, V. N.
MECHANICS OF SOLIDS, 2022, 57 (01) : 132 - 138
[9] Method for Predicting the Stability Limit to Acoustic Oscillations in Liquid-Propellant Rocket Engine Combustion Chambers Based on Combustion Noise
Biryukov, V. I.
Ivanov, V. N.
Tsarapkin, R. A.
COMBUSTION EXPLOSION AND SHOCK WAVES, 2021, 57 (01) : 74 - 82
[10] ON THE CYCLIC DEFORMATION OF THE SHELL OF THE COMBUSTION CHAMBER OF A MULTIPLE-ACTION LIQUID-PROPELLANT ROCKET ENGINE
V. S. Zarubin
V. N. Zimin
Mechanics of Solids, 2022, 57 : 132 - 138

← 1 2 →