• DocumentCode
    3028203
  • Title

    High-accuracy DNS of supersonic base flows and control of the near wake

  • Author

    Sandberg, Richard D. ; Fasel, Hermann F.

  • Author_Institution
    Dept. of Aerosp. & Mech. Eng., Arizona Univ., Tucson, AZ, USA
  • fYear
    2004
  • fDate
    7-11 June 2004
  • Firstpage
    80
  • Lastpage
    88
  • Abstract
    Large-scale numerical simulations of axisymmetric, supersonic base flows were conducted at various Reynolds numbers. Direct numerical simulations (DNS) were employed to investigate the hydrodynamic stability behavior of the near-wake region. As a consequence of physical flow instabilities, large coherent structures evolve that have a significant impact on the mean flow wand and are responsible for a considerable amount of base-drag. It is demonstrated that the deliberate exclusion or reinforcement of certain helical modes can lead to a rise in base-pressure and thus decrease the drag of a blunt body at supersonic speed. For these investigations, a high-order accurate compressible Navier-Stokes solver in cylindrical coordinates with high parallel efficiency was developed and employed on the SGI Origin 3900 shared memory complex at the ERDC MSRC. In addition to providing vital insight into the physical mechanisms in supersonic base flows, the DNS results are intended for use as benchmark data for the development of a flow simulation methodology (FSM) for high Reynolds number turbulent flows.
  • Keywords
    Navier-Stokes equations; aircraft; computational fluid dynamics; flow instability; flow simulation; numerical analysis; projectiles; supersonic flow; turbulence; wakes; Reynolds number turbulent flow; axisymmetric supersonic base flow; compressible Navier-Stokes solver; flow simulation methodology; high-accuracy direct numerical simulation; hydrodynamic stability behavior; large-scale numerical simulation; near-wake region; physical flow instability; wake control; Aerodynamics; Aerospace engineering; Hydrodynamics; Large-scale systems; Mechanical engineering; Missiles; Numerical simulation; Projectiles; Stability; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Users Group Conference (DOD_UGC'04), 2004
  • Conference_Location
    Williamsburg, VA, USA
  • Print_ISBN
    0-7695-2259-9
  • Type

    conf

  • DOI
    10.1109/DOD_UGC.2004.22
  • Filename
    1420856