Abstract
A multigrid-based calculation procedure is presented for the efficient solution of the time-averaged equations of a turbulent, elliptic-reacting flow. The equations are solved on a nonorthogonal curvilinear coordinate system. The physical models currently incorporated are a two-equation A-e turbulence model, a four-step chemical kinetics mechanism, and a Lagrangian particle-tracking procedure applicable to dilute sprays. Demonstration calculations are presented to illustrate the performance of the calculation procedure for a ramjet dump combustor configuration.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 431-437 |
| Number of pages | 7 |
| Journal | Journal of Propulsion and Power |
| Volume | 5 |
| Issue number | 4 |
| DOIs | |
| State | Published - 1989 |
| Externally published | Yes |
ASJC Scopus subject areas
- Aerospace Engineering
- Fuel Technology
- Mechanical Engineering
- Space and Planetary Science