Zobrazeno 1 - 10
of 279
pro vyhledávání: '"Yihua Cao"'
Publikováno v:
Applied Sciences, Vol 13, Iss 12, p 7214 (2023)
In this article, a degeneration method of inverse simulation is proposed for a helicopter system flying pull-up and slalom maneuvers. This inverse simulation method has been successfully applied, and here, the results are compared with the flight tes
Externí odkaz:
https://doaj.org/article/be289a98409c46b89e95382eadfd514a
Publikováno v:
Journal of Marine Science and Engineering, Vol 10, Iss 10, p 1455 (2022)
Landing a helicopter to the ship flight deck is most demanding even for the most experienced pilots and modeling and simulation of the ship-helicopter dynamic interface is a substantially challenging technical problem. In this paper, a coupling numer
Externí odkaz:
https://doaj.org/article/b36ebb1f322a458f9df45cb983f67b85
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
Sustained flight operation in the rain conditions is still a challenge to a pilot. This problem can be mainly attributed to the aerodynamic performance degradation of aircraft. In this article, in order to quickly understand the influence of rainfall
Externí odkaz:
https://doaj.org/article/295a2cdcb5f949a4b6444dc5e519ca0c
Publikováno v:
Journal of Colloid and Interface Science. 629:896-907
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cfe0442d027e544fc29eb4a221d84a92
https://doi.org/10.1016/j.jcis.2022.09.125
https://doi.org/10.1016/j.jcis.2022.09.125
Publikováno v:
Fluid Dynamics & Materials Processing. 19:1301-1315
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a99161d6037229b3a2adeeda5b795965
https://doi.org/10.32604/fdmp.2023.023435
https://doi.org/10.32604/fdmp.2023.023435
Publikováno v:
Applied Sciences, Vol 12, Iss 1, p 126 (2021)
The gas-solid two-phase flow model is constructed based on the Euler-Lagrangian framework. The SST k−ω two-equation turbulence model and the soft ball model are coupled by computational fluid dynamics (CFD) and a discrete element model (DEM). Brow
Externí odkaz:
https://doaj.org/article/fa20e05d36944fbaa8903f405265d517
Publikováno v:
Archives of Computational Methods in Engineering. 30:573-613
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bdcefef8e014aeb673662e8eb3703020
https://doi.org/10.1007/s11831-022-09808-6
https://doi.org/10.1007/s11831-022-09808-6
Publikováno v:
International Journal of Aerospace Engineering, Vol 2020 (2020)
In this paper, the multibody parachute-payload system is simplified and analyzed. A six-degree-of-freedom rigid body flight dynamic model is established to calculate the flight trajectory, attitude, velocity, and drop point of the parachute-payload s
Externí odkaz:
https://doaj.org/article/51ecb16375de4edeb03295898af9694b
Publikováno v:
Chinese Journal of Aeronautics.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e9d720f19f2d34fa88e7e21883264ee
https://doi.org/10.1016/j.cja.2023.04.027
https://doi.org/10.1016/j.cja.2023.04.027
Publikováno v:
Applied Sciences, Vol 11, Iss 11, p 5109 (2021)
This article describes the results of modeling and analysis of a generic internal cargo system using a discretization method of the vector mechanics. The model can be easily incorporated into a tandem helicopter model and is intended for use of simul
Externí odkaz:
https://doaj.org/article/4ab08b2ffe6845aa8d6ee3f4da971a0a