Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Zheng-Hong Gao"'
Publikováno v:
气体物理, Vol 8, Iss 5, Pp 19-27 (2023)
Fluidic thrust vectoring technology can provide good stealth performance and longitudinal maneuvering moment for supersonic tailless configurations, with advantages of fast response and light weight. The bypass shock vectoring nozzle does not need to
Externí odkaz:
https://doaj.org/article/c8d94fbdde1248549040d652502c4d0f
Publikováno v:
Computers & Mathematics with Applications. 141:33-41
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d64ce485ccde451d0c403aadc58de377
https://doi.org/10.1016/j.camwa.2023.03.024
https://doi.org/10.1016/j.camwa.2023.03.024
Autor:
Zheng Hong Gao, Jiren Wang
Publikováno v:
AIP Advances, Vol 11, Iss 1, Pp 015350-015350-11 (2021)
A combination of experiments and molecular simulations was used to analyze the influence of different humidity values on the adsorption of CO2 on the surface of bituminous coal. First, the fixed bed dynamic adsorption method was used. A self-develope
Externí odkaz:
https://doaj.org/article/2311d749f96445ec8e676b34a22c1aa8
Publikováno v:
Acta Astronautica. 202:442-452
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3eee14a0f805e2d39099055baeca9389
https://doi.org/10.1016/j.actaastro.2022.11.010
https://doi.org/10.1016/j.actaastro.2022.11.010
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering; Dec2023, Vol. 237 Issue 16, p3696-3708, 13p
Publikováno v:
2022 13th International Conference on Mechanical and Aerospace Engineering (ICMAE).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cce19679568cc2ab0c35bbcf02802712
https://doi.org/10.1109/icmae56000.2022.9852906
https://doi.org/10.1109/icmae56000.2022.9852906
Publikováno v:
Xibei Gongye Daxue Xuebao, Vol 38, Iss 3, Pp 580-588 (2020)
This paper focus on the wing shape related drag reduction measures of normal layout civil aircraft, through the drag reduction to improve the aircraft performance. Mainly by the laminar flow wing to reduce skin drag and weak shock wave wing to reduce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b70827dfea839f8589ad1af68eb2f17d
https://doi.org/10.1051/jnwpu/20203830580
https://doi.org/10.1051/jnwpu/20203830580
Publikováno v:
Computers & Fluids. 246:105643
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bdcdcd642ee5c658730697c7c45cecf5
https://doi.org/10.1016/j.compfluid.2022.105643
https://doi.org/10.1016/j.compfluid.2022.105643
Publikováno v:
Journal of Computational Physics. 456:111027
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89635b16b9bbddaf642a4f607032f5c3
https://doi.org/10.1016/j.jcp.2022.111027
https://doi.org/10.1016/j.jcp.2022.111027
Publikováno v:
Journal of Physics: Conference Series. 2235:012065
Hypersonic vehicle is a kind of vehicle that can fly at more than Mach 5 in the atmosphere. To solve the control problem of hypersonic vehicle, this work investigates the feasibility of hypersonic jet control surface. The numerical simulation method
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51531b35164c7424b73ca1467097b032
https://doi.org/10.1088/1742-6596/2235/1/012065
https://doi.org/10.1088/1742-6596/2235/1/012065