Zobrazeno 1 - 10
of 131
pro vyhledávání: '"Shihe, Yi"'
Publikováno v:
Light: Science & Applications, Vol 13, Iss 1, Pp 1-21 (2024)
Abstract In recent years, the demand for optical imaging and detection in hypersonic aircraft has been on the rise. The high-temperature and high-pressure compressed flow field near airborne optoelectronic devices creates significant interference wit
Externí odkaz:
https://doaj.org/article/ea77b1b30b7747ebb123b3605bbe97e3
Publikováno v:
Actuators, Vol 13, Iss 1, p 30 (2024)
The influencing characteristic for the evolution mechanism of a dynamic stall vortex structure and distributed blowing control on rotor airfoils was investigated. Based on the moving-embedded grid method, the finite volume scheme, and Roe’s FDS sch
Externí odkaz:
https://doaj.org/article/0eb45b4bee244d8ebafbfd61a30b17c8
Autor:
Guoqiang, Li, Shihe, Yi
Publikováno v:
In Energy 1 December 2020 212
Publikováno v:
Chinese Journal of Aeronautics. 36:190-200
Publikováno v:
Journal of Thermophysics and Heat Transfer. :1-10
The flowfield structure, heat flux distribution, and pressure fluctuations of the wall-mounted cylinder-induced hypersonic boundary-layer transition are investigated at a 10 deg angle of attack. Experiments are conducted in a Mach 6 low-noise wind tu
Publikováno v:
Chinese Journal of Aeronautics. 35:89-101
Publikováno v:
Acta Astronautica. 193:173-181
Publikováno v:
Journal of Thermophysics and Heat Transfer. 36:296-302
An experimental study on the effects of Backward-Facing Step (BFS) shapes was conducted in the Ma6 hypersonic wind tunnel. The step shape was changed by installing different ramps in the step corne...
Publikováno v:
Chinese Journal of Aeronautics. 35:90-97
An experimental study was conducted on turbulent separation behaviors induced by blunt fins with different sweep angles at Mach number 6.0. The Nano-particle based Planar Laser Scattering technique (NPLS) was applied to visualize the flowfield, compl
Publikováno v:
Applied optics. 61(35)
The supersonic mixing layer formed on the surface of hypersonic/supersonic flight vehicles’ optical windows is the main structure that induces aero-optical effects (AOEs), which may cause severe imaging degradation. Previous research has found that