Study on performance and mechanisms of a novel integrated model with Power & Thermal Management system and turbofan engine
• A novel integrated model is developed by combining PTMS and engine system. • An off-design heat exchanger submodule without specifying detailed geometry is embedded. • The coupling influences of PTMS and engine are revealed over the entire flight envelope. • The weak cooling performance of PTMS ar...
Ausführliche Beschreibung
Autor*in: |
Zhuang, Laihe [verfasserIn] |
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Format: |
E-Artikel |
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Sprache: |
Englisch |
Erschienen: |
2023 |
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Schlagwörter: |
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Übergeordnetes Werk: |
Enthalten in: Wind resource mapping and energy estimation in complex terrain: A framework based on field observations and computational fluid dynamics - Radünz, William Corrêa ELSEVIER, 2020, design, processes, equipment, economics, Amsterdam [u.a.] |
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Übergeordnetes Werk: |
volume:219 ; year:2023 ; day:25 ; month:01 ; pages:0 |
Links: |
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DOI / URN: |
10.1016/j.applthermaleng.2022.119481 |
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Katalog-ID: |
ELV059713860 |
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• A novel integrated model is developed by combining PTMS and engine system. • An off-design heat exchanger submodule without specifying detailed geometry is embedded. • The coupling influences of PTMS and engine are revealed over the entire flight envelope. • The weak cooling performance of PTMS arises in high Mach number and altitude regions. |
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• A novel integrated model is developed by combining PTMS and engine system. • An off-design heat exchanger submodule without specifying detailed geometry is embedded. • The coupling influences of PTMS and engine are revealed over the entire flight envelope. • The weak cooling performance of PTMS arises in high Mach number and altitude regions. |
abstract_unstemmed |
• A novel integrated model is developed by combining PTMS and engine system. • An off-design heat exchanger submodule without specifying detailed geometry is embedded. • The coupling influences of PTMS and engine are revealed over the entire flight envelope. • The weak cooling performance of PTMS arises in high Mach number and altitude regions. |
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