Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Deyuan Xu"'
Publikováno v:
Proceedings of the 11th International Conference on Biomedical Engineering and Bioinformatics.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::37267287552ae1e5a3b384ba10eacd44
https://doi.org/10.5220/0011381500003443
https://doi.org/10.5220/0011381500003443
Publikováno v:
AIAA Journal. 53:3297-3304
In the flight process of liquid-propulsion launch vehicles, coupling effect exists among vibration of rocket system, pressure, and flux oscillation of propulsion system and thrust perturbation. This effect may lead to instability or large vibration r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a2ef9b9851be595656d9792f850bca2
https://doi.org/10.2514/1.j053859
https://doi.org/10.2514/1.j053859
Publikováno v:
AIAA Journal. 53:405-412
Considering the flexibility of a liquid rocket propellant tank and the importance of the relationship between oscillatory pressure and outflow near the tank outlet, a three-dimensional modeling technique is developed to provide a more accurate tank s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::108ba9b4990cab3a751cf8e60bedc990
https://doi.org/10.2514/1.j053046
https://doi.org/10.2514/1.j053046
Publikováno v:
AIAA Journal. Feb2015, Vol. 53 Issue 2, p405-412. 8p.
Autor:
Yu Hao1,2 haoy11@fudan.edu.cn, Guo-an Tang1,3 tangguoan@fudan.edu.cn, Deyuan Xu1 xudeyuanghw@gmai1.com, Qiongliang Yang4 061029008@fudan.edu.cn
Publikováno v:
AIAA Journal. Nov2015, Vol. 53 Issue 11, p3297-3304. 8p.