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...
-д хадгалсан:
| Үндсэн зохиолчид: | , , , |
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| Формат: | Artigo |
| Хэл сонгох: | Inglês |
| Хэвлэсэн: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2018-12-01
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| Цуврал: | INCAS Bulletin |
| Нөхцлүүд: | |
| Онлайн хандалт: | http://bulletin.incas.ro/files/onel__afilipoae__neculaescu__pricop__vol_10_iss_4.pdf |
| Шошгууд: |
Шошго байхгүй, Энэхүү баримтыг шошголох эхний хүн болох!
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