Zobrazeno 1 - 10
of 63
pro vyhledávání: '"V I Zapryagaev"'
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 63:940-949
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::efa9d1fadc7bbe7354e1b4c92ddbc76c
https://doi.org/10.1134/s0021894422060049
https://doi.org/10.1134/s0021894422060049
Publikováno v:
Прикладная механика и техническая физика. 63:31-42
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b8df74f58d566815c8a8c9d63c8ee0b
https://doi.org/10.15372/pmtf20220604
https://doi.org/10.15372/pmtf20220604
Publikováno v:
Thermophysics and Aeromechanics. 28:811-820
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2f06caabf06266d0cba6f8196897184
https://doi.org/10.1134/s0869864321060056
https://doi.org/10.1134/s0869864321060056
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 61:710-716
This paper describes a study of a laminar separated flow in a compression corner for the Mach number of the incident flow M = 6 and 8. The shock-wave structure of the flow in its reattachment region is considered. The formation mechanism of a high-pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5fce97cbe7a698e171be3d970e2af741
https://doi.org/10.1134/s0021894420050041
https://doi.org/10.1134/s0021894420050041
Publikováno v:
Fluid Dynamics. 55:185-193
The paper presents the results of an experimental investigation of the mixing layer parameters in the initial regions of transonic jets issuing from convergent nozzles with different internal roughness at the same Mach number in the jet core. It is s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8be67fd3845ed97bf67a7b7dbeeaeb35
https://doi.org/10.1134/s0015462820010073
https://doi.org/10.1134/s0015462820010073
Publikováno v:
Thermophysics and Aeromechanics. 27:23-33
The present work is devoted to the experimental study of a high-speed jet exhausting from a model dual-stream jet nozzle which was performed using non-contact (shadow visualization) and probing (Pitot pressure tube) methods for measuring gas-dynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d190f600e6fed9c8df4d0640d4ebd788
https://doi.org/10.1134/s0869864320010023
https://doi.org/10.1134/s0869864320010023
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 236:477-489
In this work, results of an experimental study of the flow structure in the region of reattachment of a supersonic laminar separated flow are reported. The separated flow is generated by a model shaped as a compression corner consisting of a horizont
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fba779d86e67dfd05374c07a2a829d98
https://doi.org/10.1177/0954410018809600
https://doi.org/10.1177/0954410018809600
Publikováno v:
International Journal of Heat and Mass Transfer. 129:997-1009
The structure of a laminar separation flow around a compression corner at a free-stream Mach number M∞ = 6 is considered. The existence of a new element in the reattachment area—a high total-pressure layer—is shown. This layer is located downst
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1d20c8abb58776a973731fd92311db8
https://doi.org/10.1016/j.ijheatmasstransfer.2018.09.125
https://doi.org/10.1016/j.ijheatmasstransfer.2018.09.125
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3996aec6fecaa5d7f00ebe452f671ff4
https://doi.org/10.1063/5.0052001
https://doi.org/10.1063/5.0052001
Publikováno v:
AIP Conference Proceedings.
The work focuses on the effect of transversal runoff on the high-pressure layer in a supersonic (M = 6) separated compression corner flow. The high-pressure layer is formed behind the reattachment line of the separated flow and is characterized by hi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::319de3f4c75854b72c24e8c9aacb36da
https://doi.org/10.1063/5.0052018
https://doi.org/10.1063/5.0052018