| DOI | Resolve DOI: https://doi.org/10.2514/6.2021-2660 |
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| Author | Search for: Neuteboom, Martin1 |
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| Affiliation | - National Research Council Canada. Aerospace
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| Format | Text, Article |
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| Conference | AIAA Aviation 2021 Forum, August 2-6, 2021, Virtual Event |
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| Subject | axial compressors; aircraft engines; icing wind tunnel; surface thermocouples; heat transfer; ice clouds; static pressure; icing conditions; heat conduction; NACA 0012 |
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| Abstract | 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. Commissioning of the rig was conducted in the NRC’s altitude icing wind tunnel (AIWT) in 2019. Analysis of icing behavior categorized ice accretion into four severity levels which appeared to be dependent on a single parameter: melt-ratio. This paper presents transient analysis of metal surface temperatures for the identified icing severity levels. |
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| Publication date | 2021-08-02 |
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| Publisher | American Institute of Aeronautics and Astronautics |
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| In | |
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| Language | English |
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| Peer reviewed | Yes |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 9978bc02-620c-4c9d-9ca6-2f4b15cc9e93 |
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| Record created | 2023-01-19 |
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| Record modified | 2023-01-19 |
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