Zobrazeno 1 - 10
of 20
pro vyhledávání: '"V G, Shakhov"'
Publikováno v:
Омский научный вестник, Vol 1 (163), Pp 67-71 (2019)
Authors propose a method and algorithms for the rapid diagnosis of locomotives traction engines based on duplication of main frequency channel by additional wavelet analysis and decision — making on the methodology of fuzzy logic. The method an
Externí odkaz:
https://doaj.org/article/0aec06bf6f9f4b0dbc865716a915a37b
Publikováno v:
Офтальмохирургия, Vol 0, Iss 1, Pp 84-90 (2018)
The article summarizes the experience in the development of information technology and telemedicine at the Novosibirsk Branch of the S. Fyodorov Eye Microsurgery Federal State Institution within an improvement of the administrative-management, medica
Externí odkaz:
https://doaj.org/article/6edf780d4d624780a5619a697b2d664d
Publikováno v:
Научный вестник МГТУ ГА, Vol 21, Iss 1, Pp 30-39 (2018)
The main technical and economic characteristics of the future aircraft are introduced at the early stages of the design process. The high responsibility of these stages is explained by the necessity to make more than 70% of the conceptual decisions o
Externí odkaz:
https://doaj.org/article/eee07c9fcf1c427e9dbf4068ef703e2f
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 16, Iss 3, Pp 39-46 (2017)
The paper considers one of the stages of atmospheric entry for aerospace craft. The aim is to investigate the influence of turbulence models on aircraft aerodynamics properties. To study the influence of a turbulence model on aircraft aerodynamic pro
Externí odkaz:
https://doaj.org/article/864062759f374a78b5eddd2f06dd558b
Publikováno v:
Chinese Journal of Aeronautics, Vol 33, Iss 8, Pp 2133-2145 (2020)
The spaceplane is perspective vehicle due to wide maneuverability in comparison with a space capsule. Its maneuverability is expressed by the larger flight range and also by a possibility to rotate orbital inclination in the atmosphere by the aerodyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3784dbe313550bdf3f144ad6e6150c4d
https://doi.org/10.1016/j.cja.2020.04.016
https://doi.org/10.1016/j.cja.2020.04.016
Autor:
V. Yu. Tetter, V. G. Shakhov
Publikováno v:
Omsk Scientific Bulletin. :67-71
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::da6aa264a62dc6ab64cb8fa2c8a79d99
https://doi.org/10.25206/1813-8225-2019-163-67-71
https://doi.org/10.25206/1813-8225-2019-163-67-71
Publikováno v:
Journal of Engineering Thermophysics. 27:541-544
For the first time the limit conditional cycles in P-V and T-S coordinates of the device implementing the stratification effect (TL) for subsonic and supersonic flow regimes have been presented. The analysis of energy efficiency of heat exchange proc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b31341e9ef7d8782d12040d8a361df0d
https://doi.org/10.1134/s1810232818040161
https://doi.org/10.1134/s1810232818040161
Publikováno v:
Acta Astronautica. 148:153-162
Hypersonic flow is a very complex regime due to high values of velocity that causes air dissociation and ionization. This paper explores the influence of air dissociation on aircraft aerodynamic properties. The approach is the creation of a block-str
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d0b850910fb3c0e5d1be22a83962d75
https://doi.org/10.1016/j.actaastro.2018.05.001
https://doi.org/10.1016/j.actaastro.2018.05.001
Publikováno v:
Procedia Engineering. 185:160-167
In this work the rarefied gas flows in microchannels is investigated. With low pressure owing to low gas density the gas slippage affetcting the channel walls is observed. The task of sliding flow on initial segments of flat (two-dimensional) channel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6a91860a898e9597e419c762dea407a1
https://doi.org/10.1016/j.proeng.2017.03.334
https://doi.org/10.1016/j.proeng.2017.03.334
Publikováno v:
AIP Conference Proceedings.
The air launch is a one of way to deliver spacecraft into orbit. This paper investigates of rocket aerodynamic characteristics with influence from an aircraft. The approach is a calculation of aerodynamic characteristics for an isolated rocket and sy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff712dd8f69200f78700b65fce3d5290
https://doi.org/10.1063/1.5081547
https://doi.org/10.1063/1.5081547