Análise aero-estrutural de um demonstrador da combustão supersônica
In the current scenario of the aerospace sector, there is a great limitation related to the payload that can be launched into orbit or beyond. Rocket engines, propulsive technology in operation, have a low specific impulse compared to airbreathing propulsion systems (in general, including scramje...
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| Médium: | masterThesis |
| Jazyk: | pt_BR |
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Universidade Federal do Rio Grande do Norte
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| On-line přístup: | https://repositorio.ufrn.br/handle/123456789/51270 |
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