Simulation of turbulent swirl flow in an axisymmetric sudden expansion

Citation
By. Guo et al., Simulation of turbulent swirl flow in an axisymmetric sudden expansion, AIAA J, 39(1), 2001, pp. 96-102
Citations number
18
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
39
Issue
1
Year of publication
2001
Pages
96 - 102
Database
ISI
SICI code
0001-1452(200101)39:1<96:SOTSFI>2.0.ZU;2-F
Abstract
The numerical simulation of the turbulent flows in axisymmetric sudden expa nsions with inlet swirl is addressed, with the focus being on the unsteady flow behavior. Numerical simulations using the Reynolds-averaged Navier-Sto kes equations closed via the k-epsilon turbulence model are presented. Resu lts fur an expansion ratio of 1.96 and a Reynolds number of 1 x 10(5) (at t he inlet) are presented for a range of swirl numbers from O to 0.48. The pr ecessing vortex core (PVC) and most of the features observed experimentally , including the precession direction, zero-frequency swirl number, and vort ex breakdown have been predicted. The calculated precession frequency for t he case of an expansion ratio of 1.96 is in close agreement with that repor ted in the literature. Moreover, a higher-order oscillation, in addition to the low-frequency PVC, has been predicted over a range of swirl numbers.