| DOI | Resolve DOI: https://doi.org/10.2514/6.2020-2826 |
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| Author | Search for: Davison, Craig R.1; Search for: Chalmers, Jennifer L.1; Search for: Neuteboom, Martin1 |
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| Affiliation | - National Research Council of Canada. Aerospace
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| Format | Text, Article |
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| Conference | AIAA Aviation 2020 Forum, June 15-19, 2020, Virtual Event |
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| Physical description | 14 p. |
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| Subject | 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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| 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 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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| Publication date | 2020-06-08 |
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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 | 35e4eb19-5a6c-404d-a497-28571ecd916e |
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| Record created | 2022-03-28 |
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| Record modified | 2022-03-28 |
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