The geometric characteristics of the front and the length selection for the combustion chamber of direct flow type
A method has been developed for selecting the geometric characteristics of the front and the length of the direct-flow combustion chamber. Afterburner combustion chambers are of the ramjet type and are used for a short-term increase in the thrust of a gas turbine engine during takeoff, for overcomin...
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| Format: | article |
| Langue: | EN RU UK |
| Publié: |
National Aerospace University «Kharkiv Aviation Institute»
2021
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| Accès en ligne: | https://doaj.org/article/9393cd90f53b4fe18394405d972e19f0 |
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