Abstract
The performance of nozzle on subcritical and supercritical condition was numerical simulated. The effect of nozzle jet flowfield performance on nozzle inner flowfield was also studied. A third order Godunov type algorithm which has TVD property was employed. In order to simulate jet flow field domain decomposition method and chimeral grid was also employed. Rieman problem was constructed on zonal boundary, numerical test show that this method could treat arbitrary discontinuity from arbitrary direction well.
| Original language | English |
|---|---|
| Pages (from-to) | 53-55 |
| Number of pages | 3 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 21 |
| Issue number | 3 |
| State | Published - Mar 2000 |
| Externally published | Yes |
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