| Download | - View final version: Estimated performance of derwent V with oversize exhaust nozzles (PDF, 2.6 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003784 |
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| Author | Search for: Smith, E. L.1 |
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| Affiliation | - National Research Council of Canada. National Aeronautical Establishment
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| Format | Text, Memorandum |
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| Physical description | 6 p. |
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| Abstract | The following memorandum has been prepared to enable performance estimates to be made for a Meteor aircraft when equipped with Derwent V (or VIII) engines, fitted with reheat systems having a cold loss of about 3 percent and with various oversize exhaust nozzles. |
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| Publication date | 1953-04-08 |
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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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| 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 | c9fb07f0-c343-4f63-9ace-2e0edbae5a52 |
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| Record created | 2025-10-14 |
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| Record modified | 2025-11-03 |
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