Design of a Supersonic Wind Tunnel
This study was a preliminary work of how to implement a rocket with sensors in order to get information about the flight.
| Autores: | , , , |
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| Tipo de recurso: | informe técnico |
| Fecha de publicación: | 2011 |
| País: | España |
| Institución: | Universitat Politècnica de Catalunya (UPC) |
| Repositorio: | UPCommons. Portal del coneixement obert de la UPC |
| Idioma: | inglés |
| OAI Identifier: | oai:upcommons.upc.edu:2117/16017 |
| Acceso en línea: | https://hdl.handle.net/2117/16017 |
| Access Level: | acceso abierto |
| Palabra clave: | Wind tunnel models High-speed aeronautics Túnels aerodinàmics Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica::Tunels aerodinàmics |
| Sumario: | This study was a preliminary work of how to implement a rocket with sensors in order to get information about the flight. |
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