Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Honghui Xiang"'
Publikováno v:
Symmetry, Vol 15, Iss 9, p 1692 (2023)
Multi-output Gaussian process regression measures the similarity between samples based on Euclidean distance and assigns the same weight to each feature. However, there are significant differences in the aerodynamic performance of plane cascades comp
Externí odkaz:
https://doaj.org/article/4569da820c8348f580b29be2028beeb5
Publikováno v:
International Journal of Aerospace Engineering, Vol 2020 (2020)
In the performance test of a compressor, the overstrain alarm of a rotor blade occurred and it was thought to be caused by a large-sized inlet probe. To explain and further avoid the occurrence of this phenomenon, the influences of probe strut config
Externí odkaz:
https://doaj.org/article/1cdd20d036a74a52969d99a671217794
Autor:
Yong, Yang, Yaoming, Fu, Binbin, Lin, Kuanxin, Hou, Ling Bing, Kong, Honghui, Xiang, Jie, Gao, Shiqi, Jiang
Publikováno v:
International Journal of Turbo & Jet-Engines; 2023 Supplement 1, Vol. 40 Issue 1, ps607-s619, 13p
Autor:
Kuanxin Hou, Honghui Xiang, Jie Gao, Binbin Lin, Qiulin Dai, Yaoming Fu, Yong Yang, Lei Huang
Publikováno v:
International Journal of Turbo & Jet-Engines.
Aiming at the problem of aerodynamic coupling interference between disturbance of the built-in measurement probe and internal flow of high load compressor, the experiment of axial position and structure dimension of cylindrical probe support effect o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2119508626061dda7d470a7d2d3c787c
https://doi.org/10.1515/tjeng-2022-0027
https://doi.org/10.1515/tjeng-2022-0027
Publikováno v:
Journal of Thermal Science. 30:1674-1683
An experimental investigation was conducted in order to understand the installation effects of inlet measurement probes on the vibration characteristics of the rotor blades in two axial compressors. The vibration signal of the rotor blades was analyz
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::577766cdd48cb51ec19955b15b2a2610
https://doi.org/10.1007/s11630-021-1447-y
https://doi.org/10.1007/s11630-021-1447-y
Publikováno v:
International Journal of Aerospace Engineering, Vol 2020 (2020)
In the performance test of a compressor, the overstrain alarm of a rotor blade occurred and it was thought to be caused by a large-sized inlet probe. To explain and further avoid the occurrence of this phenomenon, the influences of probe strut config
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f3fca6098d7ddaed1f22e19926b7d77d
https://doi.org/10.1155/2020/8897211
https://doi.org/10.1155/2020/8897211
Publikováno v:
Xibei Gongye Daxue Xuebao, Vol 37, Iss 6, Pp 1223-1230 (2019)
Due to the fact that there are numerous factors and parameters associated to tandem cascade, and upstream and downstream blades have intensive interference and unknown matching correlation, it is difficult to create tandem blades with high performanc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ac02d61e3a8c6153ee89344ba3030e84
https://www.jnwpu.org/articles/jnwpu/full_html/2019/06/jnwpu2019376p1223/jnwpu2019376p1223.html
https://www.jnwpu.org/articles/jnwpu/full_html/2019/06/jnwpu2019376p1223/jnwpu2019376p1223.html
Publikováno v:
Journal of Systems Science and Information. 7:359-372
Air transportation systems are often subject to failures or attacks induced by unexpected abominable weather or temporal airspace occupation, while complex networks have been springing up as a convenient yet efficient tool to represent and analyze va
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84b0402aca55ef35581fbc4a26c53b86
https://doi.org/10.21078/jssi-2019-359-14
https://doi.org/10.21078/jssi-2019-359-14
Publikováno v:
2019 Proceedings of the Conference on Control and its Applications
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d59c66455ddfb23a966d8c4718b7ddb5
https://doi.org/10.1137/1.9781611975758.14
https://doi.org/10.1137/1.9781611975758.14
Autor:
Yong, Yang, Yaoming, Fu, Binbin, Lin, Kuanxin, Hou, Ling Bing, Kong, Honghui, Xiang, Jie, Gao, Shiqi, Jiang
Publikováno v:
International Journal of Turbo and Jet Engines; April 2022, Vol. 40 Issue: Supplement 1 ps607-s619, 13p