Change of temperature field in the depending mixing chamber on the bypass ratio
The mixing chamber of a turbofan jet engine with an additional turbofan unit is the object of this study. The subject of the research is the influence of the bypass ratio on the formation of the temperature field in the mixing chamber before the turbofan unit turbine. This study investigates how the...
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| Hauptverfasser: | , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
National Aerospace University «Kharkiv Aviation Institute»
2025-08-01
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| Schriftenreihe: | Авіаційно-космічна техніка та технологія |
| Schlagworte: | |
| Online-Zugang: | http://nti.khai.edu/ojs/index.php/aktt/article/view/3031 |
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