Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Hesen Yang"'
Autor:
Hesen Yang, Chi Zhang, Yuyang Shen, Haifeng Gao, Guifen Zhang, Wanxue Liu, Hongbo Jiang, Yibo Zhang
Publikováno v:
Insects, Vol 15, Iss 3, p 208 (2024)
Tomato is the most preferred host plant for Tuta absoluta, a newly emerged devastating invasive pest in China. However, no study has evaluated the damage risk of T. absoluta on processed tomato worldwide. In the current study, the life table paramete
Externí odkaz:
https://doaj.org/article/756d4161655e47f4a7a4d44b6a90984a
Publikováno v:
Aerospace, Vol 11, Iss 1, p 60 (2024)
The double-wedge configuration is a typical characteristic shape of the rudder surface of high-speed aircraft. The impact of the shock wave/boundary layer interaction and the shock wave/shock wave interaction resulting from the double wedge on aircra
Externí odkaz:
https://doaj.org/article/be963cba3fcf480d926ce13d87aa25b5
Publikováno v:
Aerospace, Vol 10, Iss 12, p 1016 (2023)
Compression corner shock wave/boundary layer interaction (SWBLI) is a typical shock wave/boundary layer interaction (SWBLI) problem in supersonic/hypersonic flows. In previous studies, the separation flow is usually caused by a single shock wave. How
Externí odkaz:
https://doaj.org/article/b369dfc00c0f494daf74c905ddc70f8c
Publikováno v:
Advances in Aerodynamics, Vol 3, Iss 1, Pp 1-13 (2021)
Abstract At present, the control capability of dielectric barrier discharge (DBD) plasma actuation covers the flow velocity range of helicopter’s retreating blades, so it is necessary to extend it to the dynamic stall control of rotor airfoils. A D
Externí odkaz:
https://doaj.org/article/9876e96c4bdf49c0b79f35d853ceb457
Publikováno v:
Actuators, Vol 12, Iss 6, p 229 (2023)
Crosswinds will lead to large-scale flow separation in the nacelle inlets, which seriously affects the flight safety of the aircraft; there is an urgent need to develop flow control measures. As a plasma flow control method, the application of surfac
Externí odkaz:
https://doaj.org/article/c69397c8592c4306b67d8bd43ab55f34
Plasma Actuation for the Turbulent Mixing of Fuel Droplets and Oxidant Air in an Aerospace Combustor
Publikováno v:
Aerospace, Vol 10, Iss 1, p 77 (2023)
In order to explore plasma-assisted turbulent mixing in aerospace engines, the dielectric barrier discharge plasma actuation for the turbulent mixing of fuel droplets and oxidant air in a ramjet combustor was studied using computational fluid dynamic
Externí odkaz:
https://doaj.org/article/553d13d27e77440cbe0dd250078523aa
Publikováno v:
Actuators, Vol 11, Iss 6, p 148 (2022)
This study was designed to explore the control effect of pulsed arc discharge plasma actuation on the incident shock wave/boundary layer interaction (ISWBLI). Research was conducted on an ISWBLI flow field with 10 kHz single-channel pulsed arc discha
Externí odkaz:
https://doaj.org/article/3800550639a246e5abc61ae38afbc835
Publikováno v:
Actuators; Volume 12; Issue 6; Pages: 229
Crosswinds will lead to large-scale flow separation in the nacelle inlets, which seriously affects the flight safety of the aircraft; there is an urgent need to develop flow control measures. As a plasma flow control method, the application of surfac
Autor:
Shimin Liu, Hua Liang, Haohua Zong, Hesen Yang, Jie Chen, Dongsheng Zhang, Zhi Su, Weiliang Kong
Publikováno v:
Science Progress; Oct-Dec2023, Vol. 106 Issue 4, p1-27, 27p, 6 Diagrams, 1 Chart, 9 Graphs
Autor:
Hesen Yang, Hua Liang, Chuanbiao Zhang, Yun Wu, Zhehao Li, Haohua Zong, Zhi Su, Bo Yang, Yakang Kong, Dongsheng Zhang, Yinghong Li
Publikováno v:
Physics of Fluids.
In this paper, an experimental study on the stability of hypersonic plate boundary layer is carried out using a spanwise plasma actuation array. The characteristics and evolution of different kinds of unstable waves in the hypersonic plate boundary l