| Auteur | Rechercher : Rasimarzabadi, Faezeh1; Rechercher : Neuteboom, Martin1; Rechercher : Clark, Catherine1; Rechercher : Martensson, Hans |
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| Affiliation | - Conseil national de recherches du Canada. Aérospatiale
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| Format | Texte, Article |
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| Conférence | 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021, September 6-10, 2021, Shanghai, China |
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| Sujet | aerodynamic; propulsion; boundary layer ingestion (BLI); computational fluid dynamics (CFD) |
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| Résumé | A boundary layer ingestion (BLI) test rig has been developed by National Research Council of Canada in Ottawa for studying a sub-scale BLI propulsion technology that has the potential to reduce aircraft fuel consumption by improving the propulsion efficiency of aircraft engines. This paper provides details of the aerodynamic design and analysis of the related test rig. This BLIrig is unique compared to most known projects in that it is capable of achieving representative cruise flight altitudes and Mach numbers while most other known studies have been performed at sea level and lower speeds. The results include CFD simulation of applying an ejector to get high subsonic flow at the tunnel test section, as the first option, then modifying the existing high altitude test rig at different parts, as a better option for a BLI test rig. |
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| Date de publication | 2021-09-10 |
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| Maison d’édition | The Conference |
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| Dans | |
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| Langue | anglais |
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| Publications évaluées par des pairs | Oui |
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| Exporter la notice | Exporter en format RIS |
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| Signaler une correction | Signaler une correction (s'ouvre dans un nouvel onglet) |
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| Identificateur de l’enregistrement | 6994b445-21de-47d7-8c74-119ae99c2e82 |
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| Enregistrement créé | 2023-06-16 |
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| Enregistrement modifié | 2023-06-16 |
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