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Supersonic - subsonic transition in relatively narrow channels
- 1.0211498 - UT-L 20000134 RIV CN eng J - Journal Article
Dvořák, Rudolf
Supersonic - subsonic transition in relatively narrow channels.
Journal of Thermal Science. Roč. 9, č. 4 (2000), s. 311-315. ISSN 1003-2169. E-ISSN 1993-033X
R&D Projects: GA AV ČR IAA2076901
Subject RIV: JU - Aeronautics, Aerodynamics, Aircrafts
The flow structure of supersonic-subsonic transition in relatively narrow channels has a strong 3D character with complex flow phenomena, like regions of localized separation, various vortical structures, etc. In the paper only three problems are considered: effect of channel width, transition in a pseudoshock wave, flow near the critical cross section.
Permanent Link: http://hdl.handle.net/11104/0107047
Number of the records: 1