First principles simulation of reacting hypersonic flow over a blunt wedge

被引:8
|
作者
Grover, Maninder S. [1 ,2 ]
Verhoff, Ashley M. [2 ]
Valentini, Paolo [1 ,2 ]
Bisek, Nicholas J. [2 ]
机构
[1] Univ Dayton, Res Inst, 1700 S Patterson Blvd, Dayton, OH 45409 USA
[2] US Air Force, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
CHEMICAL-KINETIC PROBLEMS; FUTURE NASA MISSIONS; DISSOCIATION; ENERGY;
D O I
10.1063/5.0161570
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This article presents molecular-level analysis of a reactive, near-continuum, Mach 21 nitrogen flow over a blunt wedge using the direct molecular simulation (DMS) method. The flow conditions lead to internal energy excitation and dissociation in the flow field, resulting in thermal and chemical nonequilibrium in the flow. Thermal nonequilibrium in the vibrational mode is observed to extend to the molecular level, where the vibrational energy distributions at various points in the flow field are observed to be non-Boltzmann. Furthermore, this is the first reactive DMS calculation where the wall is assumed to be isothermal and full momentum accommodation of the particles is enforced, hence incorporating viscous wall effects. Since the DMS method uses a quantum mechanically generated interaction potential as its only modeling input, all thermochemical and transport properties of the flow field can directly be attributed to the ab initio potential energy surface. Using the DMS solution as a benchmark, this article assesses the performance of Navier-Stokes computational fluid dynamics solutions using lower fidelity two-temperature models. Two models are chosen as points of comparison: the well-known Park two-temperature model and the recently developed modified Marrone and Treanor model.
引用
收藏
页数:17
相关论文
共 50 条
  • [31] HYPERSONIC FLOW WITH VISCOUS INTERACTION OVER A SHARP SLENDER WEDGE
    RODKIEWICZ, CM
    AIAA JOURNAL, 1974, 12 (01) : 7 - 8
  • [32] N-S/DSMC Hybrid Simulation of Hypersonic Flow over Blunt Body Including Wakes
    Li, Zhonghua
    Li, Zhihui
    Li, Haiyan
    Yang, Yanguang
    Jiang, Xinyu
    PROCEEDINGS OF THE 29TH INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS, 2014, 1628 : 519 - 526
  • [33] Modeling and simulation of turbulent reacting flow around a hypersonic space probe
    Nguyen-Bui, N. T-H.
    Duffa, G.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (04) : 919 - 923
  • [34] DUSTY HYPERSONIC WEDGE FLOW
    PEDDIESON, J
    LYU, CH
    AIAA JOURNAL, 1973, 11 (01) : 110 - 112
  • [35] HYPERSONIC FLOW PAST WEDGE
    NATH, G
    CURRENT SCIENCE, 1964, 33 (18): : 548 - &
  • [36] THE EFFECT OF THERMAL RADIATION ON THE INVISCID HYPERSONIC FLOW OVER A BLUNT BODY
    BIRD, GA
    JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09): : 713 - 714
  • [37] Numerical study of the viscous hypersonic flow over a blunt delta wing
    Gorshkov, A. B.
    COMPUTATIONAL MATHEMATICS AND MATHEMATICAL PHYSICS, 2009, 49 (09) : 1622 - 1631
  • [38] Numerical study of the viscous hypersonic flow over a blunt delta wing
    A. B. Gorshkov
    Computational Mathematics and Mathematical Physics, 2009, 49 : 1622 - 1631
  • [39] NUMERICAL METHOD FOR HYPERSONIC INTERNAL FLOW OVER BLUNT LEADING EDGES AND 2 BLUNT BODIES
    DSOUZA, N
    MOLDER, S
    MORETTI, G
    AIAA JOURNAL, 1972, 10 (05) : 617 - &
  • [40] REAL GAS EFFECTS IN FLOW OVER BLUNT BODIES AT HYPERSONIC SPEEDS
    NAGAMATSU, HT
    GEIGER, RE
    SHEER, RE
    JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (04): : 241 - 251