Zobrazeno 1 - 10
of 18
pro vyhledávání: '"O. Obraz"'
Publikováno v:
Fluid Dynamics. 58:232-239
Publikováno v:
Doklady Physics. 67:110-113
Publikováno v:
AIAA Journal. 59:3398-3405
Experiments show that a sudden expansion of supersonic flow may strongly stabilize or even relaminarize the boundary layer. Only few theoretical studies addressed this effect considering evolution ...
NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER
Autor:
Nikolay Nikolaevich Semenov, Anton O. Obraz, Ivan Vladimirovich Egorov, Andrei Valerievich Novikov, A. V. Fedorov
Publikováno v:
TsAGI Science Journal. 51:573-585
Publikováno v:
IUTAM Laminar-Turbulent Transition ISBN: 9783030679019
In this work effect of wall normal gas injection on boundary-layer stability is investigated for the high-speed flow over two models of space vehicles—the hemispherical model and the model of Exomars project. The mean flows are obtained using numer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c19ba36baca1bbf4f87f9b5e1e1ee278
https://doi.org/10.1007/978-3-030-67902-6_8
https://doi.org/10.1007/978-3-030-67902-6_8
Publikováno v:
AIP Conference Proceedings.
Publikováno v:
AIP Conference Proceedings.
Publikováno v:
Journal of Fluid Mechanics. 859:949-971
Atmospheric particulates may be a major source of boundary-layer instabilities leading to laminar–turbulent transition on aerodynamically smooth bodies flying at supersonic speeds. Particulates penetrating into the boundary-layer flow can excite wa
Publikováno v:
Computers & Fluids. 162:26-38
The generation of a turbulent spot by an unstable wave packet propagating in a Mach-6 flat-plate boundary layer is considered. The asymptotic shape of the wave packet is obtained in the far field from the excitation point using linear stability theor
Publikováno v:
International Journal of Heat and Mass Transfer. 149:119197
The wall normal gas injection effect on the heat transfer and the boundary-layer stability is investigated for the high-speed flow over hemispherical model of space vehicle. The heat flux distributions on the body surface are obtained using numerical