Supercomputer modeling of flow past hypersonic flight vehicles

被引：1
|
作者：
Ermakov, M. K. [1 ]
Kryukov, I. A. [1 ]
机构：
[1] Russian Acad Sci, A Ishlinsky Inst Problems Mech, Vernadsky Prospect 101 1, Moscow 119526, Russia
来源：
10TH INTERNATIONAL CONFERENCE ON AEROPHYSICS AND PHYSICAL MECHANICS OF CLASSICAL AND QUANTUM SYSTEMS | 2017年 / 815卷
关键词：
D O I：
10.1088/1742-6596/815/1/012016
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
A software platform for MPI-based parallel solution of the Navier-Stokes (Euler) equations for viscous heat-conductive compressible perfect gas on 3-D unstructured meshes is developed. The discretization and solution of the Navier-Stokes equations are constructed on generalized S.K. Godunov's method and the second order approximation in space and time. Developed software platform allows to carry out effectively flow past hypersonic flight vehicles simulations for the Mach numbers 6 and higher, and numerical meshes with up to 1 billion numerical cells and with up to 128 processors.
引用
收藏
页数：5
相关论文
共 50 条
  • [1] Flight Dynamics Modeling and Analysis of Flexible Hypersonic Flight Vehicles
    Tian, Xianke
    Tang, Shuo
    Zhu, Qiangjun
    [J]. APPLIED MECHANICS AND MATERIALS I, PTS 1-3, 2013, 275-277 : 513 - 517
  • [2] Aerodynamic Modeling for Hypersonic Flight Vehicles with Account of Scramjet Effects
    Hu, Shuang
    Zhu, Jihong
    [J]. 2017 IEEE INTERNATIONAL CONFERENCE ON SYSTEMS, MAN, AND CYBERNETICS (SMC), 2017, : 1657 - 1662
  • [3] Design of hypersonic flight vehicles: some lessons from the past and future challenges
    Hirschel, E. H.
    Weiland, C.
    [J]. CEAS SPACE JOURNAL, 2011, 1 (1-4) : 3 - 22
  • [4] Aeroelastic Simulation of Hypersonic Flight Vehicles
    Gupta, K. K.
    Voelker, L. S.
    [J]. AIAA JOURNAL, 2012, 50 (03) : 717 - 723
  • [5] Supercomputer modeling of parachute flight dynamics
    [J]. 2018, South Ural State University, Publishing Center (05)
  • [6] HYPERSONIC FLOW PAST WEDGE
    NATH, G
    [J]. CURRENT SCIENCE, 1964, 33 (18): : 548 - &
  • [7] On Mathematical Modeling of a Hypersonic Flow Past a Thin Wing with Variable Shape
    Bogatko, V., I
    Potekhina, E. A.
    [J]. VESTNIK ST PETERSBURG UNIVERSITY-MATHEMATICS, 2021, 54 (04) : 395 - 399
  • [8] On Mathematical Modeling of a Hypersonic Flow Past a Thin Wing with Variable Shape
    V. I. Bogatko
    E. A. Potekhina
    [J]. Vestnik St. Petersburg University, Mathematics, 2021, 54 : 395 - 399
  • [9] Simulation of 3D flows past hypersonic vehicles in Flow Vision software
    Aksenov, A. A.
    Zhluktov, S. V.
    Savitskiy, D. V.
    Bartenev, G. Y.
    Pokhilko, V. I.
    [J]. XXX INTERNATIONAL CONFERENCE ON INTERACTION OF INTENSE ENERGY FLUXES WITH MATTER (ELBRUS 2015), 2015, 653
  • [10] Integrated flight/propulsion control for unknown hypersonic flight vehicles systems
    Chen, Longsheng
    [J]. 2017 4TH INTERNATIONAL CONFERENCE ON INFORMATION, CYBERNETICS AND COMPUTATIONAL SOCIAL SYSTEMS (ICCSS), 2017, : 267 - 272
12345