Drag coefficient modelling in the context of small launcher optimisation
The purpose of this paper is to present a fast mathematical model that can be used to quickly asses the drag coefficient for generic launcher configurations. The tool developed based on this mathematical model can be used separately or it can be integrated in a multidisciplinary optimisation algorit...
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| Автори: | , , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2018-12-01
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| Серія: | INCAS Bulletin |
| Предмети: | |
| Онлайн доступ: | http://bulletin.incas.ro/files/onel__afilipoae__neculaescu__pricop__vol_10_iss_4.pdf |
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