Code-verification techniques for hypersonic reacting flows in thermochemical nonequilibrium

被引:11
|
作者
Freno, Brian A. [1 ]
Carnes, Brian R. [1 ]
Weirs, V. Gregory [1 ]
机构
[1] Sandia Natl Labs, POB 5800,MS 0828, Albuquerque, NM 87185 USA
关键词
Code verification; Hypersonic flow; Thermochemical nonequilibrium; Manufactured solutions; CHEMICAL-KINETIC PROBLEMS; FUTURE NASA MISSIONS; MANUFACTURED SOLUTIONS; VALIDATION;
D O I
10.1016/j.jcp.2020.109752
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The study of hypersonic flows and their underlying aerothermochemical reactions is particularly important in the design and analysis of vehicles exiting and reentering Earth's atmosphere. Computational physics codes can be employed to simulate these phenomena; however, verification of these codes is necessary to certify their credibility. To date, few approaches have been presented for verifying codes that simulate hypersonic flows, especially flows reacting in thermochemical nonequilibrium. In this paper, we present our code-verification techniques for verifying the spatial accuracy and thermochemical source term in hypersonic reacting flows in thermochemical nonequilibrium. We demonstrate the effectiveness of these techniques on the Sandia Parallel Aerodynamics and Reentry Code (SPARC). (C) 2020 Elsevier Inc. All rights reserved.
引用
收藏
页数:24
相关论文
共 50 条
  • [1] Thermochemical nonequilibrium modeling of oxygen in hypersonic air flows
    Kim, Jae Gang
    Kang, Sang Hun
    Park, Soo Hyung
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2020, 148 (148)
  • [2] Computation of Weakly Ionized Hypersonic Flows in Thermochemical Nonequilibrium
    Candler, Graham V.
    MacCormack, Robert W.
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 1991, 5 (03) : 266 - 273
  • [3] Numerical simulation of hypersonic thermochemical nonequilibrium blunt body flows
    Yang, Kai
    Yuan, Zhi-Chao
    Zhu, Qiang-Hua
    Gao, Xiao-Wei
    Tuijin Jishu/Journal of Propulsion Technology, 2014, 35 (12): : 1585 - 1591
  • [4] Finite element adaptive method for hypersonic thermochemical nonequilibrium flows
    AitAliYahia, D
    Habashi, WG
    AIAA JOURNAL, 1997, 35 (08) : 1294 - 1302
  • [5] Modelling dissociation in hypersonic blunt body and nozzle flows in thermochemical nonequilibrium
    Josyula, E.
    Bailey, W. F.
    SHOCK WAVES, VOL 1, PROCEEDINGS, 2009, : 653 - +
  • [6] Survey of Simulation and Diagnostic Techniques for Hypersonic Nonequilibrium Flows
    Sharma, Surendra P.
    Park, Chul
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 1990, 4 (02) : 129 - 142
  • [7] Nonlinear coupled constitutive relations for hypersonic reacting flows with thermal nonequilibrium effect
    Zeng, Shuhua
    Yang, Junyuan
    Zhao, Wenwen
    Yuan, Zhenyu
    Fan, Guochao
    Chen, Weifang
    PHYSICS OF FLUIDS, 2025, 37 (01)
  • [8] Coupled euler/boundary-layer method for nonequilibrium, chemically reacting hypersonic flows
    Wuthrich, S., 1600, Publ by AIAA, Washington, DC, United States (30):
  • [9] COUPLED EULER BOUNDARY-LAYER METHOD FOR NONEQUILIBRIUM, CHEMICALLY REACTING HYPERSONIC FLOWS
    WUTHRICH, S
    SAWLEY, ML
    AIAA JOURNAL, 1992, 30 (12) : 2836 - 2844
  • [10] THERMOCHEMICAL MODELS FOR HYPERSONIC FLOWS
    WADA, Y
    OGAWA, S
    KUBOTA, H
    COMPUTERS & FLUIDS, 1993, 22 (2-3) : 179 - 187