An investigation of the precooled turbojet engine.
The possibility of extending the range of operation of turbojet engine to hypersonic Mach number and its possible uses have been investigated. It is well known that addition or an afterburner extends the range of turbojet to Mach number of about 3. A further addition or a cooling system between ram...
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| Format: | Others |
| Language: | en |
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McGill University
1964
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| Online Access: | http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=115557 |