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Science Highlights: Advanced Scientific Computing Research and Other Projects |
Numerical Simulation of Turbulent Reacting Flows | |||||||
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Our objective is to develop and validate high-fidelity numerical models that can accurately represent both the chemical and fluid-mechanical behavior of combusting hydrocarbons in a turbulent environment.
The principal computational
tool for this project is the low Mach number adaptive mesh refinement
algorithm developed by the CCSE at NERSC. This methodology provides an
accurate and efficient approach for modeling reacting flows in the regime
that is appropriate for engineering applications. The algorithm uses a
fractional step discretization that easily facilitates the inclusion of
complex kinetics mechanisms. The methodology uses a block-structured refinement
approach that allows computational effort to be focused in regimes of
the flow where it is required. The structured refinement approach provides
a natural coarse-grained parallelism that has demonstrated excellent performance
and scalability on distributed memory architectures.
Accomplishments
During FY99, we have made substantial improvements to our methodology in two areas. In the algorithmic area, we have completed the parallelization of both the compressible and low Mach number versions of our adaptive methodology for distributed memory architectures. Computations using this methodology show that the data distribution and load balancing mechanisms we have developed provide an efficient scalable implementation of our adaptive algorithms in a framework that isolates the parallel implementation from the core physics modules for a particular application. We have also generalized the low Mach number combustion methodology to allow for arbitrarily complex chemical kinetics and transport packages using an interface to CHEMKIN. The new methodology supports complex reaction mechanisms and differential diffusion in a low Mach number formulation that conserves both species and enthalpy while maintaining second-order accuracy of the overall discretization.
The modeling of turbulent fluid flow in realistic engineering geometries, even in the non-reacting case, remains one of the great scientific challenges. For realistic combustion scenarios, the picture becomes more complex because small-scale turbulent fluctuations modify the physical processes such as kinetics and multiphase behavior. These processes, in turn, couple the small scales back to the larger fluid-dynamical scales as chemical constituents react. As a result of this coupling, we must capture the structure of the subgrid fluctuations to make predictions. The use of average quantities as inputs to physical processes will generate large errors through interaction of these models. Developing techniques that accurately reflect the role of small-scale fluctuations on the overall macroscopic dynamics would represent a major scientific breakthrough. The range of length
scales involved in practical engineering devices precludes the possibility
of a direct numerical simulation in which all the relevant length scales
are resolved. Consequently, any attempt to model realistic devices such
as engines and furnaces requires some type of turbulent combustion model
that represents the subgrid interplay between turbulence and kinetics.
The goal of this project is to develop these types of models. Publications M. S. Day and J. B. Bell, "Numerical simulation of laminar reacting flows with complex chemistry," Combust. Theory Modelling (submitted); LBNL-44682 (1999). J. B. Bell, N. J. Brown, M. S. Day, M. Frenklach, J. F. Grcar, and S. R. Tonse, "The effect of stoichiometry on vortex flame interactions," 28th Symp. (International) on Combustion (submitted); LBNL-44730 (1999). |
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