The generation of shaft power at hypersonic Mach numbers.
An analysis of the inverted gas turbine cycle applied to aircraft propulsion for the Mach Number range 0 - 6 is summarized and the shaft power potential revealed. [...]
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| Format: | Others |
| Language: | en |
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McGill University
1961
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| Online Access: | http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=118158 |
| Summary: | An analysis of the inverted gas turbine cycle applied to aircraft propulsion for the Mach Number range 0 - 6 is summarized and the shaft power potential revealed. [...] |
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