| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1715343 | Acta Astronautica | 2012 | 9 Pages |
Transverse slot injection scheme is very important for the mixing process between the air and the fuel in supersonic flows. The effect of the turbulence model and slot width on the transverse slot injection flow field has been investigated numerically based on the grid independency analysis, and the predicted results have been compared with the experimental data available in the open literature. The obtained results show that the grid scale makes only a slight difference to the wall pressure profiles for all jet-to-crossflow pressure ratios employed in this study, and the wall pressure profile with low jet-to-crossflow pressure ratio is predicted accurately by the RNG k–ε turbulence model, the SST k–ω turbulence model for the flow field with high jet-to-crossflow pressure ratio. High jet-to-crossflow pressure ratio can increase the jet penetration depth in supersonic flows, and the gradient of the length of the upstream separation region is larger than that of the height of the Mach surface. At the same time, when the jet-to-crossflow pressure ratio is maintained constant, the jet penetration depth increases with the increase of the slot width.
► Grid scale makes only a slight difference to the wall pressure profiles. ► Turbulence models for different jet-to-crossflow pressure ratios are clarified. ► Jet penetration depth increases with the increase of the slot width and the jet-to-crossflow pressure ratio.
