Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Zhang, ZhunHyok"'
Autor:
Ri, CholUk, Namgung, Hwan, Zhang, Zhunhyok, Chae, Chunghyok, Ri, Kwangil, Ho, Pongguk, Zhang, Ryong
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 95, Issue 1, pp. 62-72.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2022-0026
Autor:
Ri, CholUk, Ri, KwangChol, Zhang, ZhunHyok, Chae, ChungHyok, Zhao, Qiang, Pak, HyeIl, Kim, JaeHun, NamGung, Hwan, Kim, ChangSop
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 94, Issue 6, pp. 915-932.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-08-2021-0256
Publikováno v:
Journal of Vibration Engineering & Technologies. 10:751-765
Squeeze Film Damper plays an important role in enhancing the dynamic stability of the rotor and damping rotor vibrations and transmitted forces when traversing critical speeds. Depending on how SFD is designed, SFD can reduce the vibration and transm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94d9f0f5af2371d37d3dcda0c61786af
https://doi.org/10.1007/s42417-021-00406-7
https://doi.org/10.1007/s42417-021-00406-7
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Publikováno v:
Journal of Vibration Engineering & Technologies. 9:1433-1445
One of the main causes for failure in the rotor machine is the presence of internal cracks in the shaft rotating at high speed. The occurrence of such cracks has a dangerous and catastrophic effect on the dynamic behavior of rotating structures and c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de8dc34ed3247f5abcb60271103e39d2
https://doi.org/10.1007/s42417-021-00306-w
https://doi.org/10.1007/s42417-021-00306-w
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1441-1456
The inclusion of aerospike on blunt nose body of hypersonic vehicle has been considered to be the simplest and most efficient technique for a concurrent reduction of both aeroheating and wave drag due to hypersonic speed. However, the thermal and mec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8788a497217b9363cc8bb14645261b62
https://doi.org/10.1177/0954410020976488
https://doi.org/10.1177/0954410020976488