Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Lian-Hua Tan"'
Publikováno v:
Advances in Aerodynamics, Vol 2, Iss 1, Pp 1-11 (2020)
For internal flow with supersonic inflow boundary conditions, a complicated oblique shock reflection may occur. Different from the planar shock reflection problem, where the shape of the incident shock can be a straight line, the shape of the inciden
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::04e545e9881d6082c4aa8e748d614496
https://doi.org/10.21203/rs.3.rs-40887/v2
https://doi.org/10.21203/rs.3.rs-40887/v2
Publikováno v:
Modern Physics Letters B. 19:1511-1514
The characteristics of Mach stem in steady and unsteady Mach reflections are important in supersonic vehicle design. In this paper we give an overview of the current status of the study on the height and shape characteristics of Mach stem. Notably, w
Publikováno v:
Journal of Fluid Mechanics. 546:341
The flow fields behind the Mach stem in steady-state Mach reflections are analysed theoretically and numerically. When the angle between the slipline and the reflecting plane is sufficiently small, the subsonic flow just behind the Mach stem can be d
Publikováno v:
Journal of Fluid Mechanics; Jan2006, Vol. 546 Issue 1, p341-362, 22p