NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Parallel Simulation of Unsteady Turbulent FlamesTime-accurate simulation of turbulent flames in high Reynolds number flows is a challenging task since both fluid dynamics and combustion must be modeled accurately. To numerically simulate this phenomenon, very large computer resources (both time and memory) are required. Although current vector supercomputers are capable of providing adequate resources for simulations of this nature, the high cost and their limited availability, makes practical use of such machines less than satisfactory. At the same time, the explicit time integration algorithms used in unsteady flow simulations often possess a very high degree of parallelism, making them very amenable to efficient implementation on large-scale parallel computers. Under these circumstances, distributed memory parallel computers offer an excellent near-term solution for greatly increased computational speed and memory, at a cost that may render the unsteady simulations of the type discussed above more feasible and affordable.This paper discusses the study of unsteady turbulent flames using a simulation algorithm that is capable of retaining high parallel efficiency on distributed memory parallel architectures. Numerical studies are carried out using large-eddy simulation (LES). In LES, the scales larger than the grid are computed using a time- and space-accurate scheme, while the unresolved small scales are modeled using eddy viscosity based subgrid models. This is acceptable for the moment/energy closure since the small scales primarily provide a dissipative mechanism for the energy transferred from the large scales. However, for combustion to occur, the species must first undergo mixing at the small scales and then come into molecular contact. Therefore, global models cannot be used. Recently, a new model for turbulent combustion was developed, in which the combustion is modeled, within the subgrid (small-scales) using a methodology that simulates the mixing and the molecular transport and the chemical kinetics within each LES grid cell. Finite-rate kinetics can be included without any closure and this approach actually provides a means to predict the turbulent rates and the turbulent flame speed. The subgrid combustion model requires resolution of the local time scales associated with small-scale mixing, molecular diffusion and chemical kinetics and, therefore, within each grid cell, a significant amount of computations must be carried out before the large-scale (LES resolved) effects are incorporated. Therefore, this approach is uniquely suited for parallel processing and has been implemented on various systems such as: Intel Paragon, IBM SP-2, Cray T3D and SGI Power Challenge (PC) using the system independent Message Passing Interface (MPI) compiler. In this paper, timing data on these machines is reported along with some characteristic results.
Document ID
19960021012
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Menon, Suresh
(Georgia Inst. of Tech. Atlanta, GA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-CR-200892
NAS 1.26:200892
Report Number: NASA-CR-200892
Report Number: NAS 1.26:200892
Accession Number
96N24505
Funding Number(s)
CONTRACT_GRANT: N00014-92-J-4030
CONTRACT_GRANT: N00014-95-1-0163
CONTRACT_GRANT: NAG3-1610
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available