TY - GEN
T1 - High-accuracy DNS of supersonic base flows and control of the near wake
AU - Sandberg, Richard D.
AU - Fasel, Hermann F.
PY - 2004
Y1 - 2004
N2 - 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 bas -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.
AB - 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 bas -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.
UR - http://www.scopus.com/inward/record.url?scp=21444443024&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=21444443024&partnerID=8YFLogxK
U2 - 10.1109/dod_ugc.2004.22
DO - 10.1109/dod_ugc.2004.22
M3 - Conference contribution
AN - SCOPUS:21444443024
SN - 0769522599
SN - 9780769522593
T3 - Proceedings - Department of Defense High Performance Computing Modernization Program Users Group Conference, UGC 2004
SP - 80
EP - 88
BT - Proceedings - Users Group Conference, UGC 2004
PB - IEEE Computer Society
T2 - DoD HPCMP Users Group Conference, UGC 2004
Y2 - 7 June 2004 through 11 July 2004
ER -