Hypersonic nonequilibrium aerothermodynamics in CFD-FASTRAN

被引：0
|
作者：
Zhang, Sijun [1 ]
Blosch, Ed [1 ]
机构：
[1] ESI CFD Inc, Huntsville, AL 35806 USA
来源：
FEDSM 2007: PROCEEDINGS OF THE 5TH JOINT AMSE/JSME FLUIDS ENGINEERING SUMMER CONFERENCE VOL 1, PTS A AND B | 2007年
关键词：
CFD; two-temperature; hypersonic; non-equilibrium; aerothermodynamics;
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This paper presents the implementation of a state of the art Navier-Stokes code CFD-FASTRAN capable of simulating flow in thermochemical non-equilibrium. CFD-FASTRAN models the fluid as a reacting gas in chemical and thermal non-equilibrium using standard finite rate chemistry models and a two-temperature model for the gas. To validate, a code-to-code comparison between LAURA code and CFD-FASTRAN was carried out.
引用
收藏
页码：1843 / 1852
页数：10
相关论文
共 50 条
  • [31] COMPARISON OF HYPERSONIC EXPERIMENTS AND PNS PREDICTIONS .1. AEROTHERMODYNAMICS
    BHUTTA, BA
    LEWIS, CH
    JOURNAL OF SPACECRAFT AND ROCKETS, 1991, 28 (04) : 376 - 386
  • [32] Surrogate Models for Hypersonic Aerothermodynamics and Aerodynamics using Gaussian Process Regression
    Rataczak, Jens A.
    Boyd, Iain D.
    McMahon, Jay W.
    AIAA SCITECH 2024 FORUM, 2024,
  • [33] SIMULATION OF NONEQUILIBRIUM HYPERSONIC FLOWS
    RIEDEL, U
    MAAS, U
    WARNATZ, J
    COMPUTERS & FLUIDS, 1993, 22 (2-3) : 285 - 294
  • [34] Aerodynamic configuration optimization by the integration of aerodynamics, aerothermodynamics and trajectory for hypersonic vehicles
    Yi Feng
    Wei Tang
    Yewei Gui
    ChineseScienceBulletin, 2014, 59 (33) : 4608 - 4615
  • [35] Aerothermodynamics of a 1.6-meter-diameter sphere in hypersonic rarefied flow
    Dogra, V.K., 1789, (30):
  • [36] Aerothermodynamics of a Blunt Airfoil with a Flow-Through Duct for Hypersonic Flight
    Yadav, Rajesh
    Faisal, Mohammad
    Minglani, Dheeraj
    FLUID MECHANICS AND FLUID POWER - CONTEMPORARY RESEARCH, 2017, : 125 - 134
  • [37] Aerothermodynamics of hypersonic small nose cone with local rarefied gas effects
    Wang, Zhihui
    Bao, Lin
    Jisuan Wuli/Chinese Journal of Computational Physics, 2010, 27 (01): : 59 - 64
  • [38] AEROTHERMODYNAMICS OF A 1.6-METER-DIAMETER SPHERE IN HYPERSONIC RAREFIED FLOW
    DOGRA, VK
    WILMOTH, RG
    MOSS, JN
    AIAA JOURNAL, 1992, 30 (07) : 1789 - 1794
  • [39] Aerodynamic configuration optimization by the integration of aerodynamics, aerothermodynamics and trajectory for hypersonic vehicles
    Feng, Yi
    Tang, Wei
    Gui, Yewei
    CHINESE SCIENCE BULLETIN, 2014, 59 (33): : 4608 - 4615
  • [40] Rapid prediction of global hypersonic vehicle aerothermodynamics based on adaptive sampling
    Yang G.
    Yue Z.
    Liu L.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2023, 44 (06):
12345