Selection of gas turbine exit unit geometry with minimum pressure losses
Object and purpose of research. This paper discusses gas turbine exit unit consisting of axial-radial diffusor and pockettype volute. The purpose of the study was to select the exit unit geometry that would offer minimum losses of total pressure. Subject matter and methods. Experimental results obt...
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| Format: | Article |
| Language: | English |
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Krylov State Research Centre
2022-10-01
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| Series: | Труды Крыловского государственного научного центра |
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| Online Access: | https://transactions-ksrc.ru/eng/archive/selection-of-gas-turbine-exit-unit-geometry-with-minimum-pressure-losses/ |