Zobrazeno 1 - 10
of 96
pro vyhledávání: '"Xiaoqing Qiang"'
Publikováno v:
Aerospace, Vol 10, Iss 3, p 226 (2023)
The moving endwall has a great influence on the development and stability of axial compressor leakage flow. This paper presents a novel experimental facility with a high-speed moving endwall for studying axial compressor leakage flow. The uniqueness
Externí odkaz:
https://doaj.org/article/dc9162f64cba421499a8392e6f7b3c2c
Publikováno v:
Advances in Mechanical Engineering, Vol 13 (2021)
This paper focuses on the effect of hub clearance in the design space of the highly loaded cantilevered stator. The embedded 1.5 stages of a low-speed research compressor (LSRC) were conducted with Unsteady Reynolds Average Navier-Stokes (URANS) nume
Externí odkaz:
https://doaj.org/article/31fd5169b6be4854a0c99205acf84dc5
Publikováno v:
Aerospace Systems. 6:107-118
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 237:402-417
The paper describes the film cooling characteristics of the trench film hole fed by the internal cross-flow. Three internal cross-flow cases are investigated by using numerical simulations. Results show that the main flow structures of the smooth and
Publikováno v:
Aerospace Systems. 5:491-501
Autor:
Yaoyao Qu, Xiaoqing Qiang
Publikováno v:
Lecture Notes in Electrical Engineering ISBN: 9789819906505
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a39c7757ad28f0898ee13cd531db3ae5
https://doi.org/10.1007/978-981-99-0651-2_12
https://doi.org/10.1007/978-981-99-0651-2_12
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy (Sage Publications, Ltd.); Mar2023, Vol. 237 Issue 2, p402-417, 16p
Publikováno v:
Journal of Shanghai Jiaotong University (Science).
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 236:420-434
A steady and unsteady numerical research is carried out to explore some effects of a specific non-axisymmetric tip clearance layout on the overall performance and stability of an axial compressor stage. For a 4-stage low-speed research compressor (LS
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 236:1577-1589
While the consistent advance in computational power has enabled the Computational Fluid Dynamics (CFD) an effective tool for compressor performance characterization, the need for quick performance estimates at initial design phase of compressor still