Modeling three-dimensional gas-turbine combustor model flow using second-moment closure

Journal Article · Fri Jul 01 04:00:00 EDT 1994 · AIAA Journal

DOI:https://doi.org/10.2514/3.12210· OSTI ID:45793

Lin, C A; Lu, C M ^[1]

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1. Natl. Tsing Hua Univ., Hsinchu (China)

Numerical predictions were applied to a gas-turbine combustor model flow where dilutions jets were injected radially inwards into a swirling flow, leading to a very strong interaction between the two streams. Effects of different inlet swirl level to the interior flowfield were investigated numerically, and the predicted mean and turbulence results were also contrasted with measurements. The present study demonstrates that the characteristics of the combustor flow are closely linked to the representation of the interaction between the swirl field and the jets. Diffusive transport was found to be highly influential, and this also increases the importance of turbulence representation. Comparisons with experimental measurements indicated that the stress model with an anisotropy modified epsilon source combined with quadratic approximation of convection fluxes represents the flowfield reasonably well, in contrast to the k-epsilon model whose diffusive nature leads to an intense vortex core near the centerline region. Reduction of strength of the centerline recirculation zone due to the elevated level of swirl momentum transport from the swirler was also well reproduced by the stress model variant. 17 refs.

• Sponsoring Organization: USDOE
• OSTI ID: 45793
• Journal Information: AIAA Journal, Journal Name: AIAA Journal Journal Issue: 7 Vol. 32; ISSN AIAJAH; ISSN 0001-1452
• Country of Publication: United States
• Language: English

Related Subjects

32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION
42 ENGINEERING
COMBUSTION CHAMBERS
COMPUTERIZED SIMULATION
STRESS ANALYSIS
TURBULENT FLOW
VORTICES