Finite volume algorithm to compute dense compressible gas-solid flows

Citation
L. Combe et Jm. Herard, Finite volume algorithm to compute dense compressible gas-solid flows, AIAA J, 37(3), 1999, pp. 337-345
Citations number
26
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
37
Issue
3
Year of publication
1999
Pages
337 - 345
Database
ISI
SICI code
0001-1452(199903)37:3<337:FVATCD>2.0.ZU;2-4
Abstract
A finite volume scheme is presented that allows the performance of numerica l simulations of a four-equation compressible two-fluid model on unstructur ed meshes. The convective part of the whole set of governing equations is a nonconservative conditionally hyperbolic system. To solve the latter, a fr actional step method is presented, which is based on a splitting of convect ive fluxes. Approximate Roe-type Riemann solvers are used to compute numeri cal convective fluxes. Some computations of shock-tube test cases are prese nted and compared with numerical results of a three-equation model, which a ssumes equal velocities within each phase. A steady computation of a gas-so lid flow in a simple nozzle is described, and an unsteady computation of a dense fluidized bed is also presented, Particular emphasis is given to the preservation of the maximum principle for the volumetric fraction.