Studies of turbojet engines for hypersonic propulsion.
This thesis contains the results of a theoretical analysis of the performance of an inverted turbojet cycle as a thrust power unit. This system is compared with a conventional turbojet with and without reheat and pre-cooling. Within the limitations of the analysis it is seen that the domain of air b...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en |
| Published: |
McGill University
1961
|
| Subjects: | |
| Online Access: | http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=113538 |