Parametric Research and Aerodynamic Characteristic of a Two-Stage Transonic Compressor for a Turbine Based Combined Cycle Engine
This paper researches the parametric optimization of a two-stage transonic compressor having a large air bypass at partial rotating speed according to flow analysis for a turbine-based combined cycle engine (TBCC). To obtain adequate thrust, the inlet transonic compressor of the turbofan part of the...
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| Format: | Article |
| Language: | English |
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MDPI AG
2022-06-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/9/7/346 |