NUMERICAL MODELIZATION OF A COMBUSTION-CHAMBER BY AN ASSEMBLY OF ELEMENTARY REACTORS

Citation
D. Capdeville et al., NUMERICAL MODELIZATION OF A COMBUSTION-CHAMBER BY AN ASSEMBLY OF ELEMENTARY REACTORS, Acta astronautica, 34, 1994, pp. 183-193
Citations number
NO
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00945765
Volume
34
Year of publication
1994
Pages
183 - 193
Database
ISI
SICI code
0094-5765(1994)34:<183:NMOACB>2.0.ZU;2-9
Abstract
Present numerical 2D (TEACH) or 3D (DIAMANT) codes, solving average Na vier-Stokes equations, give mean flow characterisation within a combus tor. This paper presents some developments using numerical tracers in order to modelize the turbulent internal flow inside a combustor as an association of elementary reactors: Perfectly Stired Reactor (PSR) an d Plug Flow Reactor (PFR). By the resolution of a scalar transport equ ation it was possible to modelize the tracer behaviour. This first ste p of the study has shown that the scheme used was very important. This transport equation has been used to compute the mean residence time o f the gas phase in some zone of interest in different geometries (2D p lane, 2D axisymmetric, 3D). These results will be compared with experi mental results. Additional techniques have been developped to compute the mass flow rate between elementary reactors. Finally, these techniq ues will be applied to a real combustion chamber modelization.