Zobrazeno 1 - 6
of 6
pro vyhledávání: '"L. P. Trubitsyna"'
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:
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
Publikováno v:
HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2019): Proceedings of the XXVI Conference on High-Energy Processes in Condensed Matter, dedicated to the 150th anniversary of the birth of S.A. Chaplygin.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a880d12c382bd4c5e0bb4f2102a5113
https://doi.org/10.1063/1.5117438
https://doi.org/10.1063/1.5117438
Publikováno v:
Journal of Physics: Conference Series. 1404:012101
The reattachment zone structure of a supersonic separated ramp flow was experimentally studied at M∞ = 6. Several ramp model configurations with and without side walls were considered. It was found that the geometric size of streamwise vortices in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc53a0051e9bad86623355e45938f822
https://doi.org/10.1088/1742-6596/1404/1/012101
https://doi.org/10.1088/1742-6596/1404/1/012101
Publikováno v:
Journal of Physics: Conference Series. 1382:012049
This article presents the study results for heat transfer in supersonic laminar separated compression corner flow. The study was carried out for free-stream Mach number M = 6 and the compression ramp angle in the range of φ = 20° – 40°.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5c83d4ad36d68c3c3282bbb4aefcbb2
https://doi.org/10.1088/1742-6596/1382/1/012049
https://doi.org/10.1088/1742-6596/1382/1/012049