Zobrazeno 1 - 10
of 93
pro vyhledávání: '"Xingmin GUI"'
Publikováno v:
Propulsion and Power Research, Vol 12, Iss 4, Pp 505-522 (2023)
Non-axisymmetric endwall contouring has been proved to be an effective flow control technique in turbomachinery. Several different flow control mechanisms and qualitative design strategies have been proposed. The endwall contouring mechanism based on
Externí odkaz:
https://doaj.org/article/244ddf71060540f0a3583b6481c7f830
Publikováno v:
Aerospace, Vol 10, Iss 3, p 207 (2023)
Inlet distortion detrimentally affects the aerodynamic performance and lessens the stability of compressors, and has received considerable attention. The need to accurately estimate its effect on the performance and stability of compressor as early a
Externí odkaz:
https://doaj.org/article/218dfb47ca0443bfb82b378cdf677556
Publikováno v:
International Journal of Turbo & Jet-Engines; May2024, Vol. 41 Issue 2, p347-361, 15p
Publikováno v:
The International Journal of Artificial Organs. 46:215-225
Background: Cardiac functions and support modes of left ventricular assist device (LVAD) will influence the pump inner flow field and blood damage potential. Methods: Computational fluid dynamics (CFD) method and lumped-parameter-model (LPM) were app
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::062a440c0408b9abeb3168a348b52ad9
https://doi.org/10.1177/03913988231155938
https://doi.org/10.1177/03913988231155938
Publikováno v:
Chinese Journal of Aeronautics. 35:74-84
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15e57a7b680b7255c3037720dfdbbe4c
https://doi.org/10.1016/j.cja.2022.05.013
https://doi.org/10.1016/j.cja.2022.05.013
Publikováno v:
Applied Sciences, Vol 11, Iss 9, p 3937 (2021)
The seal cavity leakage flow has a considerable impact on the performance of the aeroengine, especially on the multistage compressor. Thus, a quasi-three-dimensional simulation program named CAM is developed basing on circumferentially averaged throu
Externí odkaz:
https://doaj.org/article/48a71f9d6e394c658d328acd2b7c7fb6
Publikováno v:
Journal of Thermal Science. 31:1682-1695
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c61131c79ab259ee29fa3a501af68a8
https://doi.org/10.1007/s11630-022-1608-7
https://doi.org/10.1007/s11630-022-1608-7
Publikováno v:
Applied Sciences, Vol 11, Iss 1, p 422 (2021)
Gas turbine engines are highly intricate machines, and every component of them is closely associated with one another. In the traditional engine developing process, vast experiment tests are needed. To reduce unnecessary trials, a whole gas turbine e
Externí odkaz:
https://doaj.org/article/e534345bf5544f77bb1274c432f94de9
Publikováno v:
Applied Sciences, Vol 11, Iss 2, p 780 (2021)
In order to investigate the effect of seal cavity leakage flow on a compressor’s performance and the interaction mechanism between the leakage flow and the main flow, a one-stage compressor with a cavity under the shrouded stator was numerically si
Externí odkaz:
https://doaj.org/article/51578f74f212477faf43573d10e29af2
Publikováno v:
International Journal of Turbo & Jet-Engines; 2023 Supplement 1, Vol. 40 Issue 1, ps565-s581, 17p