Zobrazeno 1 - 10
of 209
pro vyhledávání: '"Y. Galerkin"'
Publikováno v:
Universidad Nacional de Ingeniería
Repositorio Institucional-UNI
UNI-Tesis
instacron:UNI
Repositorio Institucional-UNI
UNI-Tesis
instacron:UNI
En este trabajo presentamos un estudio numérico del problema de valor en la frontera con condiciones de tipo Dirichlet asociado a la Ecuación Diferencial Ordinaria(EDO) de tipo Sturm-Liouville. Los objetivos de esta investigación son el estudio de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3056::a486a78dfc52c9e3427f002edcfc0429
http://cybertesis.uni.edu.pe/handle/uni/4189
http://cybertesis.uni.edu.pe/handle/uni/4189
Publikováno v:
Universidad Nacional Pedro Ruiz Gallo
Repositorio institucional-CONCYTEC
UNPRG-Institucional
instacron:UNPRG
Repositorio institucional-CONCYTEC
UNPRG-Institucional
instacron:UNPRG
En la presente tesis se da ha conocer el uso de elementos del análisis funcional en el modelamiento y simulación de la deformación de la membrana elástica bajo la acción de una fuerza, con determinadas condiciones. Para Modelar y Simular, inicia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3056::65e9316581f121279752320d9d2cd461
Autor:
Shamsutdinov, E.V., Vankov, Yu.V., Sergeev, V.V., Rekstin, A., Semenovskiy, V., Soldatova, K., Galerkin, Y., Sokolov, K.
Publikováno v:
E3S Web of Conferences; 2019, Vol. 124, p1-5, 5p
Autor:
Y. Galerkin, O. Solovieva
Parameters of flow are calculated in vaneless diffusers with relative width 0,014–0,10. Inlet angles of flow and similarity criteria were varied. There is information on flow separation, boundary layer development, configuration of streamlines. Pol
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::21b60971d40690361c7805df05fc018d
Autor:
K. Soldatova, Y. Galerkin
A loading factor performance is necessary for the modeling of centrifugal compressor gas dynamic performance curve. Measured loading factors are linear function of a flow coefficient at an impeller exit. The performance does not depend on the compres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1a36d7aac5218cbc42e4b4f41a3a46d3
Autor:
Wu, Xiaolei1 (AUTHOR) 20131096@llu.edu.cn, Yan, Yubin2 (AUTHOR) y.yan@chester.ac.uk
Publikováno v:
Mathematics (2227-7390). Nov2024, Vol. 12 Issue 22, p3579. 27p.
Autor:
Y. Galerkin, A. Drozdov
Publikováno v:
ASME 2015 Gas Turbine India Conference.
Laboratory “Gas dynamics of turbo machines” (LGDTM) has quite effective optimal design computer programs based on theoretic analysis and experimental data. The authors do not share an opinion that 3D impellers are superior in any case. A lot of d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92e80c9199f081303b16cea77656aca3
https://doi.org/10.1115/gtindia2015-1213
https://doi.org/10.1115/gtindia2015-1213
Autor:
Y. Galerkin, L. Marenina
Stator elements «Vane diffuser + crossover + return channel» of stages with different specific speed were investigated by CFD calculations. The regime parameter was introduced to present efficiency and loss coefficient performance of all elements t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::372b92afff550fec19ee96bc1a4cd8b5
The 6th version of Universal modeling method for centrifugal compressor stage calculation is described. Identification of the new mathematical model was made. As a result of identification the uniform set of empirical coefficients is received. The ef
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::097caf0027cb1198ccf318d93e854893
Universal modeling method well proven for industrial compressors was applied for design of the high flow rate supersonic stage. Results were checked by ANSYS CFX and NUMECA Fine Turbo calculations. The impeller appeared to be very effective at transo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c993f54efdde3974540941426342aa9c