| Download | - View final version: Gas turbine cycle calculations: dual-stream reheat combustor with compound nozzle for an afterburning turbofan engine (PDF, 8.6 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003826 |
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| Author | Search for: Cockshutt, E. P.1; Search for: Rudnitski, D. M.1 |
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| Affiliation | - National Research Council of Canada. Division of Mechanical Engineering
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| Format | Text, Memorandum |
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| Physical description | 43 p. |
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| Abstract | A dual-stream combustor for a reheated turbofan engine fitted with a compound convergent nozzle is compared with separate stream and mixed stream combustors. In a computer evaluation, it was found that the performance of this configuration is slightly better than the separate stream combustor, but not as good as the mixed stream combustor. |
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| Publication date | 1972-06 |
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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 | e41fec85-6e5a-4ed7-a9e6-ffd09ae320c5 |
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| Record created | 2025-10-29 |
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| Record modified | 2025-11-03 |
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