NUMERICAL STUDY OF HIGH-TEMPERATURE NONEQUILIBRIUM AIR NOZZLE FLOW WITH STATE-TO-STATE MODEL

被引:0
|
作者
Wang H. [1 ]
Zeng M. [1 ]
Duan X. [1 ]
Wang D. [1 ]
Liu W. [1 ]
机构
[1] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
关键词
high enthalpy wind tunnel; nozzle flow; state-to-state model; thermochemical nonequilibrium; vibrational population distribution;
D O I
10.6052/0459-1879-23-471
中图分类号
学科分类号
摘要
Using state-to-state model, quasi-one-dimensional nozzle flow of high-temperature nonequilibrium air is investigated numerically. The five chemical species mixture N2/O2/NO/N/O is considered with 61 bound vibrational levels for N2, 46 for O2, and 48 for NO. Each vibrational state is regarded as a pseudo species, which leads to a total of 157 species for the air mixture. The state-specific transition rate coefficients of some processes, which have no available data, are calculated based on the relaxation time and the rate coefficients of other similar processes. The flow simulation and analysis are made for reservoir temperature from 2000 to 8000 K and pressure from 1 to 20 MPa. The nozzle flow is essentially in equilibrium before the throat, but deviates from equilibrium shortly after the throat. The mass fraction of chemical species, populations of lower energy levels, and vibrational temperatures are frozen in the downstream not far away from the throat. The vibrational temperature of N2 is freezing earlier and has a higher frozen value than that of NO and O2. The process of vibration–translation (VT) energy exchange is predominant for vibrational transition, the recombination reaction generates molecules preferably to middle vibrational levels. Throughout the nonequilibrium and frozen zone, the vibrational population distributions are far from Boltzmann distribution at vibrational temperature, and feature a large overpopulation of the high-lying vibrational levels. Increasing the reservoir pressure could reduce the nonequilibrium to a certain extent and delay the flow thermochemical freezing. © 2024 Chinese Society of Theoretical and Applied Mechanics. All rights reserved.
引用
收藏
页码:1377 / 1394
页数:17
相关论文
共 55 条
  • [1] Wang Yunpeng, Jiang Zonglin, A review of theories and methods for hypersonic nozzle design, Advances in Mechanics, 51, 2, pp. 257-294, (2021)
  • [2] Teixeira O, Pascoa J., Catalytic wall effects for hypersonic nozzle flow in thermochemical non-equilibrium, Acta Astronautica, 203, pp. 48-59, (2023)
  • [3] Gu S, Hao J, Wang Q, Et al., Influence of thermochemical nonequilibrium on expansion tube air test conditions: A numerical study, Physics of Fluids, 35, 3, (2023)
  • [4] Park C, Lee SH., Validation of multitemperature nozzle flow code, Journal of Thermophysics and Heat Transfer, 9, 1, pp. 9-16, (1995)
  • [5] Capitelli M, Armenise I, Gorse C., State-to-state approach in the kinetics of air components under re-entry conditions, Journal of Thermophysics and Heat Transfer, 11, 4, pp. 570-578, (1997)
  • [6] Park C., Review of chemical-kinetic problems of future nasa missions. I-earth entries, Journal of Thermophysics and Heat Transfer, 7, 3, pp. 385-398, (1993)
  • [7] Candler GV., Rate effects in hypersonic flows, Annual Review of Fluid Mechanics, 51, 1, pp. 379-402, (2019)
  • [8] Wang X, Hong Q, Hu Y, Et al., On the accuracy of two-temperature models for hypersonic nonequilibrium flow, Acta Mechanica Sinica, 39, 2, (2022)
  • [9] Yang X., State-to-state dynamics of elementary bimolecular reactions, Annual Review of Physical Chemistry, 58, pp. 433-459, (2007)
  • [10] Pan TJ, Stephani KA., Rovibrationally state-specific collision model for the O<sub>2</sub>(sigmag-3) + O(p<sup>3</sup>) system in dsmc, The Journal of Chemical Physics, 154, 10, (2021)