Modeling of Processes in the Combustion Chamber of a Hybrid Solid-Fuel Engine

被引:1
|
作者
Stamov, L. I. [1 ,2 ]
Tyurenkova, V. V. [1 ,2 ]
Mikhalchenko, E. V. [1 ,2 ]
Chen, F. [3 ]
Meng, Yu. [3 ]
机构
[1] Russian Acad Sci, Natl Res Ctr Kurchatov Inst, Sci Res Inst Syst Anal, Moscow, Russia
[2] Lomonosov Moscow State Univ, Fac Mech & Math, Chair Wave & Gas Dynam, Moscow, Russia
[3] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai, Peoples R China
关键词
hybrid engines; solid fuel; numerical simulation; combustion; regression rate;
D O I
10.3103/S0027133024700134
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper presents the results of three-dimensional computational modeling of processes in the combustion chamber of a hybrid solid-fuel engine. Polymethylmethacrylate was used as a solid fuel, and air was used as an oxidizer. In the model used, the heated oxidizer in gaseous form was fed into the combustion chamber at supersonic speed. As a result of the interaction of the oxidizer with the surface of the solid fuel, it begins to warm up and decompose with the release of flammable gases. The geometry of the combustion chamber and solid fuel was based on experimental work. The results of a series of calculations for various geometries of the combustion chamber were presented. The distribution of physical parameters corresponding to the diffusion mode of combustion was obtained.
引用
收藏
页码:97 / 101
页数:5
相关论文
共 50 条
  • [1] Combustion stability in a solid-fuel ramjet engine
    Rashkovskiy, S. A.
    Yakush, S. E.
    Baranov, A. A.
    11TH INTERNATIONAL CONFERENCE AEROPHYSICS AND PHYSICAL MECHANICS OF CLASSICAL AND QUANTUM SYSTEMS (APHM-2017), 2018, 1009
  • [2] MODELING SOLID-FUEL RAMJET COMBUSTION
    NETZER, DW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1977, 14 (12) : 762 - 766
  • [3] Numerical Simulation of Combustion in Combustion Chamber of Solid-Fuel Ramjet
    Lin Xiaodi
    Wu Xiaosong
    Xia Qiang
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 1097 - 1100
  • [4] Influence of the Structure of a Solid-Fuel Mixture on the Thermal Efficiency of the Combustion Chamber of an Engine System
    Futko S.I.
    Koznacheev I.A.
    Ermolaeva E.M.
    Journal of Engineering Physics and Thermophysics, 2014, 87 (6) : 1313 - 1321
  • [5] Modeling of the Turbulent Combustion in Solid-fuel Ramjet
    Gong, Lunkun
    Chen, Xiong
    Musa, Omer
    POWER AND ENERGY SYSTEMS ENGINEERING, (CPESE 2017), 2017, 141 : 267 - 272
  • [6] APERIODIC INSTABILITY OF PROCESSES IN A SOLID-FUEL ROCKET ENGINE
    GOSTINTSEV, YA
    MARSHAKOV, VN
    SUKHANOV, LA
    LEBEDEV, PI
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1976, 12 (05) : 696 - 698
  • [7] Flight overloading effect on the working-process instability in the combustion chamber of a solid-fuel rocket engine
    Davydov, YM
    Davydova, IM
    Egorov, MY
    DOKLADY PHYSICS, 2004, 49 (09) : 527 - 529
  • [8] Flight overloading effect on the working-process instability in the combustion chamber of a solid-fuel rocket engine
    Yu. M. Davydov
    I. M. Davydova
    M. Yu. Egorov
    Doklady Physics, 2004, 49 : 527 - 529
  • [9] SOLID-FUEL SUPERSONIC COMBUSTION
    ANGUS, WJ
    WITT, MA
    LAREDO, D
    NETZER, DW
    RECHERCHE AEROSPATIALE, 1993, (06): : 1 - 8
  • [10] MODELING SOLID-FUEL RAMJET COMBUSTION, INCLUDING RADIATION TO THE FUEL SURFACE
    METOCHIANAKIS, ME
    NETZER, DW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1983, 20 (04) : 405 - 406