| DOI | Trouver le DOI : https://doi.org/10.2514/6.2020-2826 |
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| Auteur | Rechercher : Davison, Craig R.1; Rechercher : Chalmers, Jennifer L.1; Rechercher : Neuteboom, Martin1 |
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| Affiliation | - Conseil national de recherches du Canada. Aérospatiale
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| Format | Texte, Article |
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| Conférence | AIAA Aviation 2020 Forum, June 15-19, 2020, Virtual Event |
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| Description physique | 14 p. |
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| Sujet | axial compressors; icing wind tunnel; icing conditions; aircraft engines; heat and mass transfer; freestream velocity; air flowing; rotor blades; gas turbine; turbofan |
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| Résumé | The National Research Council of Canada (NRC) has developed the Ice-Crystal Environment Modular Axial Compressor Rig (ICE-MACR) for simulating altitude ice crystal icing of aircraft engines in altitude facilities. Commissioning of the rig under altitude icing conditions was conducted in the NRC’s altitude icing wind tunnel (AIWT) in May-June 2019. This paper examines the water content at the inlet and in the test section of the rig. A compact isokinetic probe was used to determine the total water content and a new version of Science Engineering Associates multi-element probe was used to differentiate water phase. In addition, a particle imaging system was used to determine particle size but also provided insight into whether the particles were in a solid or liquid state. These results will be compared to those from the multi-element probe. |
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| Date de publication | 2020-06-08 |
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| Maison d’édition | American Institute of Aeronautics and Astronautics |
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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 | 35e4eb19-5a6c-404d-a497-28571ecd916e |
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| Enregistrement créé | 2022-03-28 |
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| Enregistrement modifié | 2022-03-28 |
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