| DOI | Resolve DOI: https://doi.org/10.4224/40003763 |
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| Author | Search for: Bird, J. W.1; Search for: MacLeod, J. D.1 |
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| Affiliation | - National Research Council Canada. Division of Mechanical Engineering
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| Format | Text, Technical Report |
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| Physical description | 65 p. |
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| Abstract | Participants in the AGARD Uniform Engine Test Program installed various inlet ducting upstream of the reference airmeter and engine. In general, the resulting inlet flows exhibited thicker boundary layers than observed at NRCC. Extensive engine performance data were taken with NRCC's baseline inlet and also a smaller inlet with higher Mach number airmeter followed by a divergent duct. Temperature and pressure profile shapes at the engine face and at the compressor exit were studied. Significant calculated inlet pressure differences were measured resulting in airflow differences. However, no other significant changes in engine performance were observed. |
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| Publication date | 1987-04 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Note | The content is temporarily unavailable |
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| Language | English |
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| Peer reviewed | No |
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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 | eb8c92aa-e2ce-49b9-918a-e91615a9a605 |
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| Record created | 2025-10-01 |
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| Record modified | 2025-11-26 |
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