On the use of Boussinesq approximation in turbulent supersonic jet modeling

被引:6
|
作者
Rodionov, Alexander V.
机构
[1] Central Research Institute for Machine Building (TSNIIMASH), Korolev, Moscow Region 141070
关键词
Turbulent jets; Compressible flows; Shock waves; Reynolds-averaged; Navier-Stokes equations; Boussinesq approximation; Numerical simulations; UNDEREXPANDED JETS; PREDICTION; GODUNOV;
D O I
10.1016/j.ijheatmasstransfer.2009.11.035
中图分类号
O414.1 [热力学];
学科分类号
摘要
The problem Of turbulent supersonic jet modeling within the limits of Reynolds-averaged Navier-Stokes equations and Boussinesq approximation was considered. The time-asymptotic technique for full Navier-Stokes equations and the space-marching technique for parabolized Navier-Stokes equations were used to solve this problem A variety Of turbulence models was applied in an effort to obtain a good consistency with the experimental data on two distinct features of non-isobaric jets, namely, the mean flow decay and the shock wave attenuation It was revealed that the Boussinesq approximation in its general form used in the full Navier-Stokes equations fails to reproduce these two features together As regards the parabolized Navier-Stokes equations, such an abbreviated form gets practically rid of this failure A solid theoretical interpretation of this effect Was found, whereupon new forms Of the turbulent viscosity terms were proposed and analyzed. It was ascertained that they offer considerable advantages over the Boussinesq approximation in some CFD applications. (C) 2009 Elsevier Ltd All rights reserved
引用
收藏
页码:889 / 901
页数:13
相关论文
共 50 条
  • [21] COMBUSTION OF A TURBULENT SUPERSONIC NONISOBARIC HYDROGEN JET IN AN ACCOMPANYING SUPERSONIC AIR-FLOW
    BARANOVSKII, SI
    NADVORSKII, AS
    PERMINOV, VA
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1986, 22 (04) : 399 - 403
  • [22] COMBUSTION OF A TURBULENT SUPERSONIC NONISOBARIC HYDROGEN JET IN AN ACCOMPANYING SUPERSONIC AIR FLOW.
    Baranovskii, S.I.
    Nadvorskii, A.S.
    Perminov, V.A.
    1600, (22):
  • [23] Experimental investigation on transverse jet penetration into a supersonic turbulent crossflow
    MingBo Sun
    ShunPing Zhang
    YanHui Zhao
    YuXin Zhao
    JianHan Liang
    Science China Technological Sciences, 2013, 56 : 1989 - 1998
  • [24] Comparative Numerical Investigation of a Sonic Jet in a Supersonic Turbulent Crossflow
    Eberhardt, S.
    Hickel, S.
    HIGH PERFORMANCE COMPUTING IN SCIENCE AND ENGINEERING'14: TRANSACTIONS OF THE HIGH PERFORMANCE COMPUTING CENTER, STUTTGART (HLRS) 2014, 2015, : 351 - 366
  • [25] Experimental investigation on transverse jet penetration into a supersonic turbulent crossflow
    SUN MingBo
    ZHANG ShunPing
    ZHAO YanHui
    ZHAO YuXin
    LIANG JianHan
    Science China(Technological Sciences), 2013, 56 (08) : 1989 - 1998
  • [26] SOME LASER VELOCIMETER MEASUREMENTS IN TURBULENT WAKE OF A SUPERSONIC JET
    FLACK, RD
    THOMPSON, HD
    AIAA JOURNAL, 1977, 15 (10) : 1507 - 1509
  • [27] Turbulent characteristics of a transverse supersonic jet in a subsonic compressible crossflow
    Beresh, S.J. (sjberes@sandia.gov), 1600, American Inst. Aeronautics and Astronautics Inc. (43):
  • [28] Turbulent characteristics of a transverse supersonic jet in a subsonic compressible crossflow
    Beresh, SJ
    Henfling, JF
    Erven, RJ
    Spillers, RW
    AIAA JOURNAL, 2005, 43 (11) : 2385 - 2394
  • [29] Computation of supersonic turbulent flowfield with secondary jet normal to freestream
    Nippon Kikai Gakkai Ronbunshu, B, 615 (3595-3602):
  • [30] Turbulent structures in a supersonic jet-mixing layer interaction
    Collin, E
    Brand, P
    Delville, J
    Engineering Turbulence Modelling and Experiments 6, 2005, : 491 - 499