| Download | - View final version: Failure of compressor diffuser ring blading on Derwent mark 8-40 serial number 10653 (PDF, 1.7 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003899 |
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| Author | Search for: Wickham, V. H.1 |
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| Affiliation | - National Research Council Canada. National Aeronautical Establishment
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| Format | Text, Memorandum |
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| Physical description | 6 p. |
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| Abstract | This engine has been used for a variety of tests mostly concerned with reheat, and has been operated usually at conditions near or at the take-off rating. |
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| Publication date | 1955-06-05 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Identifier | NAE-251 |
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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 | 873119d6-282f-46db-bdc5-8a405ede4e71 |
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| Record created | 2025-11-27 |
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| Record modified | 2025-11-27 |
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