TY - GEN
T1 - Newton's method for steady and unsteady reacting flows
AU - Wensheng, Shen
AU - Jun, Zhang
AU - Fuqian, Yang
PY - 2006
Y1 - 2006
N2 - This paper describes the application of Newton's method to low Mach number steady and unsteady laminar diffusion flames, which are characterized by low flow speed and highly variable density. The newly-emerged vorticity-velocity formulation of the Navier-Stokes equations is used for both steady and unsteady compressible flows to avoid staggered mesh discretization. The nonlinear Navier-Stokes equations are discretized using finite difference method, and a secondorder backward Euler scheme is applied for the time derivatives. Central difference is used for diffusion terms to achieve better accuracy, and a monotonicity-preserving upwind difference is used for convective ones. We use an unequal-sized single grid mesh for unsteady flow and a three level multigrid method for steady flow. The coupled nonlinear system is solved via the damped Newton's method for both steady and unsteady flows. The Newton Jacobian matrix is formed numerically, and the resulting linear system is ill-conditioned and is solved by the iterative solver Bi-CGSTAB with a Gauss-Seidel preconditioner.
AB - This paper describes the application of Newton's method to low Mach number steady and unsteady laminar diffusion flames, which are characterized by low flow speed and highly variable density. The newly-emerged vorticity-velocity formulation of the Navier-Stokes equations is used for both steady and unsteady compressible flows to avoid staggered mesh discretization. The nonlinear Navier-Stokes equations are discretized using finite difference method, and a secondorder backward Euler scheme is applied for the time derivatives. Central difference is used for diffusion terms to achieve better accuracy, and a monotonicity-preserving upwind difference is used for convective ones. We use an unequal-sized single grid mesh for unsteady flow and a three level multigrid method for steady flow. The coupled nonlinear system is solved via the damped Newton's method for both steady and unsteady flows. The Newton Jacobian matrix is formed numerically, and the resulting linear system is ill-conditioned and is solved by the iterative solver Bi-CGSTAB with a Gauss-Seidel preconditioner.
KW - Diffusion flame
KW - Iterative solver
KW - Newton's method
UR - http://www.scopus.com/inward/record.url?scp=34248341329&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=34248341329&partnerID=8YFLogxK
U2 - 10.1145/1185448.1185621
DO - 10.1145/1185448.1185621
M3 - Conference contribution
AN - SCOPUS:34248341329
SN - 1595933158
SN - 9781595933157
T3 - Proceedings of the Annual Southeast Conference
SP - 756
EP - 757
BT - Proceedings of the 44th ACM Southeast Conference, ACMSE 2006
T2 - 44th Annual ACM Southeast Conference, ACMSE 2006
Y2 - 10 March 2006 through 12 March 2006
ER -