Computational study of flow separation in truncated ideal contour nozzles under high-altitude conditions
Flow separation in rocket nozzles has been studied mostly under sea-level conditions, which fail to take into account changes in ambient density and ambient pressure during the flight of a rocket. In the present study, numerical analysis is conducted of flow characteristics within a truncated ideal...
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| Autori principali: | , , , , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
AIP Publishing LLC
2024-02-01
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| Serie: | International Journal of Fluid Engineering |
| Accesso online: | https://pubs.aip.org/hgmri/ijfe/article-pdf/doi/10.1063/5.0190399/19982293/013101_1_5.0190399.pdf |
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