Performance and Exergy analysis of TurboJet and TurboFan configurations with Rotating Detonation Combustor
Conventional gas turbine is reaching its saturation level and further improvement in the cycle efficiency is possible through redesigning the cycle. One of the effective methods is to introduce a Pressure Gain Combustor (PGC) in place of the conventional deflagration combustor as PGC contributes to...
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| Autors principals: | , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
Elsevier
2024-08-01
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| Col·lecció: | International Journal of Thermofluids |
| Matèries: | |
| Accés en línia: | http://www.sciencedirect.com/science/article/pii/S2666202724001812 |
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