A Method for Design of Silo Ejector Concerning with Wall Friction

被引:0
|
作者
Quan H. [1 ]
Xie J. [1 ]
Xie Z. [2 ]
Li L. [1 ]
机构
[1] Military Key Laboratory for Armament Launch Theory & Technology, Rocket Army Engineering University, Xi'an
[2] The Rocket Force Engineering Designing Academy, Beijing
关键词
Characteristic curve; Ejector function; Silo; Stagnation critical point; Static pressure matching function; Wall friction;
D O I
10.15918/j.tbit1001-0645.2000.029
中图分类号
学科分类号
摘要
Aiming at the problem of silo design, a quasi-one dimensional method concerning with wall friction was proposed based on the ejector function method. A mathematical model of wall friction was proposed and ejector functions and static pressure matching functions concerning with wall friction were established. The analysis results prove that the velocity at the stagnation critical point is less than sonic speed, the stagnation critical point of ejector can be achieved and the third critical point is impossible to achieve. And then, the characteristics were analyzed with practical examples, considering the engine total pressure, the cross-sectional area of the silo and the outlet pressure of the mixing chamber changed respectively, and the characteristic curves were drawn. The flow patterns of supersonic jet ejectors were analyzed by CFD method, considering respectively the engine total pressure, the cross-sectional area of the silo and the outlet pressure of the mixing chamber changed. At the same time, the inlet pressures of ejectors obtained by CFD were compared with that obtained by the quasi-one dimensional method. The results show that the errors between the CFD method and the quasi-one dimensional method are little on characteristic curves and their largest value is 4.31% when the backpressure changes, which verified the quasi-one dimensional method. © 2021, Editorial Department of Transaction of Beijing Institute of Technology. All right reserved.
引用
收藏
页码:274 / 285
页数:11
相关论文
共 16 条
  • [1] WANG Fei, YANG Shuxing, XU Yong, Numerical simulation and analysis on W-type silo launching environment, Journal of Solid Rocket Technology, 30, 6, pp. 466-469, (2007)
  • [2] LIAO Daxiong, Principle and design of gas ejector, pp. 1-30, (2018)
  • [3] DAHMANI A, AIDOUN Z, GALANIS N., Optimum design of ejector refrigeration systems with environmentally benign fluids, International Journal of Thermal Sciences, 50, 8, pp. 1562-1572, (2011)
  • [4] SAMAKE O, GALANIS N, SORIN M., Thermodynamic study of multi-effect thermal vapour-compression desalination systems, Energy, 72, pp. 69-79, (2014)
  • [5] XING M, YU J, LIU X., Thermodynamic analysis on a two-stage transcritical CO<sub>2</sub> heat pump cycle with double ejectors, Energy Convers Manage, 88, pp. 677-683, (2014)
  • [6] ENGINES J., Numerical and experimental flow visualizations of the mixing process inside an induced air ejector, International Journal of Turbo Jet Engineering, 78, pp. 71-78, (2002)
  • [7] ZHU Y, JIANG P., Experimental and analytical studies on the shock wave length in convergent and convergent-divergent nozzle ejectors, Energy Convers Manage, 88, pp. 907-914, (2014)
  • [8] GALANIS N, SORIN M., Ejector design and performance prediction, International Journal of Thermal Sciences, 104, pp. 315-329, (2016)
  • [9] HASSANAMIN A, ELBADAWY I, ELGENDY E, Et al., Effect of geometrical factors interactions on design optimization process of a natural gas ejector, Advances in Mechanical Engineering, 11, 9, (2019)
  • [10] LU W, CHEN H., Design of cylindrical mixing chamber ejector according to performance analyses, Energy, 164, pp. 594-601, (2018)