The Implication of Injection Locations in an Axisymmetric Cavity-Based Scramjet Combustor
This paper presents the effect of cavity-based injection in an axisymmetric supersonic combustor using numerical investigation. An axisymmetric cavity-based angled and transverse injections in a circular scramjet combustor are studied. A three-dimensional Reynolds-averaged Navier–Stokes (RANS) equat...
| Κύριοι συγγραφείς: | , , |
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| Μορφή: | Άρθρο |
| Γλώσσα: | English |
| Έκδοση: |
MDPI AG
2021-05-01
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| Σειρά: | Energies |
| Θέματα: | |
| Διαθέσιμο Online: | https://www.mdpi.com/1996-1073/14/9/2626 |