On flow field of the system of supersonic jets in the Mars atmosphere

被引：0
|
作者：
Deryugin, Yu N. [1 ]
Zelensky, D. K. [1 ]
Zhuchkov, R. N. [1 ]
Yemel'yanova, Y., V [1 ]
Pavlov, G. A. [2 ]
Smirnov, A. L. [2 ]
机构：
[1] Russian Sci Res Inst Expt Phys, Sarov 607190, Russia
[2] RAS, Inst Problems Chem Phys, Chernogolovka 142432, Moscow Region, Russia
来源：
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER | 2019年 / 134卷
关键词：
Brakes - Supersonic aerodynamics - Mass transfer - Exhaust gases;
D O I：
10.1016/j.ijheatmasstransfer.2019.01.086
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
The paper simulates a structure and processes of heat and mass transfer in the system of exhaust jets of space vehicle brake motors during descent in the atmosphere of Mars. It is taken into account that the jet system is a chemically reacting gas medium formed by exhaust gases and atmosphere of the planet at sufficiently high temperatures and is characterized by developed turbulence. For realistic conditions the calculated fields of the complete set of parameters of the medium formed by the system of interacting supersonic exhaust jets of brake motors of the descent vehicle in the atmosphere of the planet are obtained. The parameters of the flow field in the most characteristic areas of the system of interacting jets are presented. (C) 2019 Elsevier Ltd. All rights reserved.
引用
收藏
页码：1084 / 1090
页数：7
相关论文
共 50 条
  • [1] Flow control in supersonic flow field based on micro jets
    Liu, Yanming
    Zhang, Hong
    Liu, Pingchao
    ADVANCES IN MECHANICAL ENGINEERING, 2019, 11 (01)
  • [2] Simulation of Characteristics of a System of Supersonic Jets in Carbon Dioxide Atmosphere
    Yu. N. Deryugin
    D. K. Zelenskii
    R. N. Zhuchkov
    Ya. V. Emel’yanova
    G. A. Pavlov
    A. L. Smirnov
    Technical Physics Letters, 2018, 44 : 1145 - 1149
  • [3] Simulation of Characteristics of a System of Supersonic Jets in Carbon Dioxide Atmosphere
    Deryugin, Yu. N.
    Zelenskii, D. K.
    Zhuchkov, R. N.
    Emel'yanova, Ya. V.
    Pavlov, G. A.
    Smirnov, A. L.
    TECHNICAL PHYSICS LETTERS, 2018, 44 (12) : 1145 - 1149
  • [4] NEAR-FIELD FLOW OF SUPERSONIC SWIRLING JETS
    CUTLER, AD
    LEVEY, BS
    KRAUS, DK
    AIAA JOURNAL, 1995, 33 (05) : 876 - 881
  • [5] 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
  • [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] Interaction of a system of supersonic jets from a body with an incoming flow
    Shevchenko, A., V
    Yuriev, A. S.
    Poniaev, S. A.
    Yu, Pirogov S.
    Zhitnikov, T. A.
    Rotermel, A. R.
    INTERNATIONAL CONFERENCE PHYSICA.SPB/2019, 2019, 1400
  • [8] Gas–Dynamic Structures in Supersonic Combustion of Hydrogen in a System of Plane Jets in a Supersonic Flow
    U. K. Zhapbasbaev
    E. P. Makashev
    Journal of Applied Mechanics and Technical Physics, 2001, 42 (1) : 21 - 27
  • [9] Three-dimensional flow field and acoustics of supersonic rectangular jets
    Sellappan, Prabu
    Alvi, Farrukh S.
    EXPERIMENTS IN FLUIDS, 2022, 63 (01)
  • [10] Three-dimensional flow field and acoustics of supersonic rectangular jets
    Prabu Sellappan
    Farrukh S. Alvi
    Experiments in Fluids, 2022, 63
12345