Supersonic-subsonic transition in relatively narrow channels

0211618 - UT-L 20000014 RIV CN eng C - Konferenční příspěvek (zahraniční konf.)
Dvořák, Rudolf
Supersonic-subsonic transition in relatively narrow channels.
Collected abstracts. Thermal and Fluid Sciences. Beijing: University of Beijing, 2000, s. 32-33.
[Millennium International Symposium on Thermal and Fluid Sciences. Xi´an, (CN), 18.09.2000-22.09.2000]
Grant CEP: GA AV ČR IAA2076901
Klíčová slova: shock waves * channel flow * internal aerodynamics
Kód oboru RIV: BK - Mechanika tekutin

Flow structure in relatively narrow channels has a strong 3D character with complex flow phenomena, incl. regions of localized separation, various vortical structures, etc., all of which have to be considered when dealing with the problem of supersonic-subsonic transition. three problems were considered: the effect of channel width, transition in a pseudoshock wave, flow near the critical cross section.
Trvalý link: http://hdl.handle.net/11104/0107167