Zobrazeno 1 - 10
of 64
pro vyhledávání: '"Guoqiang Yue"'
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 237:230-241
In order to obtain the effect of endwall secondary flow on the swirling film cooling, a geometric model of cascade is established to research the endwall swirling film cooling and swirling flow induced by prismatic jet impingement configurations. Num
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4fabb4329296e25c73b161e44986975
https://doi.org/10.1177/09544100221097527
https://doi.org/10.1177/09544100221097527
Publikováno v:
International Journal of Thermal Sciences. 186:108088
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5457ca7bec4be34f8cd85e1eebcf54e
https://doi.org/10.1016/j.ijthermalsci.2022.108088
https://doi.org/10.1016/j.ijthermalsci.2022.108088
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 235:1394-1405
In this paper, a hexagonal prism inlet chamber is used to form a swirling flow for the film cooling, and three kinds of compound angle of film hole ( γ = 10°, 20°, 30°) with clockwise swirling or counterclockwise swirling are used for numerical s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce477969e6f0c34585f01bb92ab0ff26
https://doi.org/10.1177/0957650921997633
https://doi.org/10.1177/0957650921997633
Publikováno v:
International Journal of Energy Research. 45:11791-11806
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3842ae76943d83f50ec72c92ebf61439
https://doi.org/10.1002/er.5749
https://doi.org/10.1002/er.5749
Publikováno v:
Applied Thermal Engineering. 223:120014
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::492f03951092115b1177bda195c5f380
https://doi.org/10.1016/j.applthermaleng.2023.120014
https://doi.org/10.1016/j.applthermaleng.2023.120014
Publikováno v:
Aerospace Science and Technology. 92:258-268
Trailing edge mixing flows associated with coolant injection are complex, in particular at transonic flows, and result in significant aerodynamics losses. A series of tests and calculations on a high-pressure turbine vane cascade with trailing edge i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73c06d45cebb8ab4caf056ebdd141707
https://doi.org/10.1016/j.ast.2019.05.069
https://doi.org/10.1016/j.ast.2019.05.069
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 233:974-987
The flows in the power turbine and nonaxisymmetric exhaust volute with struts are closely coupled and inherently unsteady for marine gas turbines, and the flow interactions between them have a significant influence on the rotor and strut blade aerody
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e667e7b2834177f9c33abeca0793fee
https://doi.org/10.1177/0957650919839583
https://doi.org/10.1177/0957650919839583
Publikováno v:
SCIENTIA SINICA Technologica. 49:753-766
In view of rotationally-induced unsteady rim sealing flow issues in the absence of mainflow nonuniform pressure fields, the large eddy simulation method validated by the enclosed rotating cavity flow measurement was adopted to investigate the instabi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53309a3dcce9ec2f670d5939e064637a
https://doi.org/10.1360/n092018-00337
https://doi.org/10.1360/n092018-00337
Evaluation on the flow characteristics of helium working fluid in generation Ⅳ nuclear power station
Publikováno v:
Nuclear Engineering and Design. 389:111667
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f539238e0ad2ddad4d89faa1176c735a
https://doi.org/10.1016/j.nucengdes.2022.111667
https://doi.org/10.1016/j.nucengdes.2022.111667
Publikováno v:
International Journal of Turbo & Jet-Engines. 39:277-289
In this study, the thickness of water film, which is frequently formed on compressor blade surface, was investigated. Simultaneously, its movement and extra torque demand were provided by a simulation model of the code. Having taken into account the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c820581639f62ad3eb2f90b1cb508c2b
https://doi.org/10.1515/tjj-2018-0027
https://doi.org/10.1515/tjj-2018-0027