Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Sidali HAIF"'
Publikováno v:
INCAS Bulletin, Vol 16, Iss 2, Pp 3-15 (2024)
The aim of this paper is to develop a profile of axisymmetric minimum length nozzle giving a uniform and parallel flow at the exit section. The study is done at high temperature, lower than the dissociation threshold of the molecules. The design is m
Externí odkaz:
https://doaj.org/article/6c693f1385f046ad82364459f0218bd3
Publikováno v:
INCAS Bulletin, Vol 15, Iss 2, Pp 33-47 (2023)
Altitude-adapted nozzles are designed to facilitate flow adaptation during rocket ascent in the atmosphere, without requiring mechanical activation. As a consequence, the performance of the nozzle is significantly improved. The aim of this study is t
Externí odkaz:
https://doaj.org/article/c17cd5aba76b4c2babfc3c98279b3f2c
Publikováno v:
Advances in Military Technology. 17:17-32
The purpose of this study is to simulate the flow in the plug nozzle. Further, the evolution of the parameters of this flow was studied. The mass of the nozzle and of the exhaust gases was calculated by the simulation. In addition, all these results
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40d96e311f7d13c515d33f1a087525fa
https://doi.org/10.3849/aimt.01523
https://doi.org/10.3849/aimt.01523