TY - JOUR
T1 - Partially reflecting and non-reflecting boundary conditions for simulation of compressible viscous flow
AU - Polifke, Wolfgang
AU - Wall, Clifton
AU - Moin, Parviz
N1 - Funding Information:
The ideas presented in this work were developed during the 2002 Summer Program of the Center for Turbulence Research (CTR) at NASA Ames Research Ctr./Stanford University [13] . Discussions with Summer Program participants and CTR staff, in particularAndre Kaufmann, Thierry Poinsot, Laurent Selle and Sanjiva Lele are gratefully acknowledged. Thanks to Andreas Huber for proof-reading and helpful suggestions. Financial support was provided by Alstom Power and Siemens Power Generation in the framework of the AG Turbo Programme (German Ministry for Education and Research) as well as by the Center for Turbulence Research.
PY - 2006/3/20
Y1 - 2006/3/20
N2 - For numerical simulation of compressible viscous flow, the characteristics-based NSCBC boundary conditions proposed by Poinsot and Lele [T. Poinsot, S.K. Lele, Boundary conditions for direct simulation of compressible viscous flows, J. Comput. Phys. 101 (1992) 104-129] are frequently employed. This formulation is analyzed analytically and it is found that the linear relaxation term proposed by Rudy and Strikwerda [D.H. Rudy, J.C. Strikwerda, A nonreflecting outflow boundary condition for subsonic Navier-Stokes calculations, J. Comput. Phys. 36 (1) (1980) 55-70] to suppress slow "drift" of flow variables results in a non-zero reflection coefficient for acoustic waves. Indeed, although the NSCBC formulation of boundary conditions is often called "non-reflecting", the magnitude of the reflection coefficient approaches unity for low frequencies. A modification of the NSCBC boundary conditions and in particular the linear relaxation term is proposed, which should appear fully non-reflecting to plane acoustic waves with normal incidence on the boundaries for all frequencies. The new formulation is implemented and successfully validated in large eddy simulation of turbulent channel flow.
AB - For numerical simulation of compressible viscous flow, the characteristics-based NSCBC boundary conditions proposed by Poinsot and Lele [T. Poinsot, S.K. Lele, Boundary conditions for direct simulation of compressible viscous flows, J. Comput. Phys. 101 (1992) 104-129] are frequently employed. This formulation is analyzed analytically and it is found that the linear relaxation term proposed by Rudy and Strikwerda [D.H. Rudy, J.C. Strikwerda, A nonreflecting outflow boundary condition for subsonic Navier-Stokes calculations, J. Comput. Phys. 36 (1) (1980) 55-70] to suppress slow "drift" of flow variables results in a non-zero reflection coefficient for acoustic waves. Indeed, although the NSCBC formulation of boundary conditions is often called "non-reflecting", the magnitude of the reflection coefficient approaches unity for low frequencies. A modification of the NSCBC boundary conditions and in particular the linear relaxation term is proposed, which should appear fully non-reflecting to plane acoustic waves with normal incidence on the boundaries for all frequencies. The new formulation is implemented and successfully validated in large eddy simulation of turbulent channel flow.
KW - Acoustics
KW - Boundary conditions
KW - Computational fluid dynamics
KW - Wave propagation and reflection
UR - http://www.scopus.com/inward/record.url?scp=31744451014&partnerID=8YFLogxK
U2 - 10.1016/j.jcp.2005.08.016
DO - 10.1016/j.jcp.2005.08.016
M3 - Article
AN - SCOPUS:31744451014
SN - 0021-9991
VL - 213
SP - 437
EP - 449
JO - Journal of Computational Physics
JF - Journal of Computational Physics
IS - 1
ER -