FLOW SIMULATION AT SHOCK WAVE TRIPLE POINT
The paper presents supersonic flow simulation results concerning the λ-foot formation in the divergent nozzle. The SPARC code was used and the vicinity of the triple point was analysed. Special boundary conditions have been used in order to obtain supersonic inlet velocity with shock wave in the di...
| Published in: | TASK Quarterly |
|---|---|
| Main Authors: | , , |
| Format: | Article |
| Language: | English |
| Published: |
Gdańsk University of Technology
2001-10-01
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| Subjects: | |
| Online Access: | https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2279 |