收藏切换
DECOUPLING OF UNSTEADY FLOW IN IMPELLER OF sCO2 CENTRIFUGAL COMPRESSOR AS TURBINE
收藏切换
PDF
Miao Senchun, Ou Yi, Wu Jiangbo, Shen Zhengjing, Wang Xiaohui, Du Xiaoze
Acta Energiae Solaris Sinica | 2026, 47(6) : 93 - 101
Less
收藏切换
Acta Energiae Solaris Sinica | 2026, 47(6): 93-101
DECOUPLING OF UNSTEADY FLOW IN IMPELLER OF sCO2 CENTRIFUGAL COMPRESSOR AS TURBINE
Full
Miao Senchun, Ou Yi, Wu Jiangbo, Shen Zhengjing, Wang Xiaohui, Du Xiaoze
Affiliations
doi: 10.19912/j.0254-0096.tynxb.2025-0153
Outline
收藏切换
In order to study the high dimensional unsteady flow characteristics in the flow field of supercritical carbon dioxide centrifugal compressor reversed as turbine, the research object is centrifugal compressor reversed as turbine, the CFX flow field analysis software was utilized for numerical simulation, the dynamic mode decomposition(DMD) was performed on the simulated results, and the first four order modes and their corresponding spatio-temporal information are obtained. The analysis results show that the DMD method can decompose the unsteady flow field into modes with distinct energy levels and frequencies, including the basic mode with the highest energy contribution (0 Hz), the dynamic and static interference mode with the second-highest energy (at the blade passing frequency), and the high order harmonic characteristics of the dynamic and static interference modes with lower energy contributions(at multiples of the blade passing frequency); The main characteristics of the basic mode are caused by the geometric parameters of the impeller, the main characteristics of the dynamic and static interference modes are caused by the dynamic and static interference between the impeller and the guide vane, and the high order harmonic characteristics of the dynamic and static interference modes show the subtle flow characteristics in the flow field; Under low-flow conditions, the first order mode exhibits a relative liquid flow angle smaller than the inlet blade angle, leading to flow separation on the pressure side of the blade inlet; Under high-flow conditions, the relative liquid flow angle of the first-order mode exceeds the inlet blade angle, resulting in flow impingement on the pressure side and flow separation on the suction side of the blade inlet. The DMD method can effectively decouple the unsteady flow field within the impeller and extract transient flow characteristics.
energy storage  /  centrifugal compressor as turbine  /  supercritical carbon dioxide  /  dynamic mode decomposition  /  impellers  /  unsteady flow
Miao Senchun, Ou Yi, Wu Jiangbo, Shen Zhengjing, Wang Xiaohui, Du Xiaoze. DECOUPLING OF UNSTEADY FLOW IN IMPELLER OF sCO2 CENTRIFUGAL COMPRESSOR AS TURBINE[J]. Acta Energiae Solaris Sinica, 2026 , 47 (6) : 93 -101 . DOI: 10.19912/j.0254-0096.tynxb.2025-0153
Year 2026 volume 47 Issue 6
PDF
86
6
Cite this Article
BibTeX
Article Info
doi: 10.19912/j.0254-0096.tynxb.2025-0153
  • Receive Date:2025-01-21
  • Online Date:2026-07-17
Article Data
Affiliations
History
  • Received:2025-01-21
Affiliations
References
Share
https://castjournals.cast.org.cn/joweb/tynxb/EN/10.19912/j.0254-0096.tynxb.2025-0153
Share to
QR

Scan QR to access full text

Cite this article
BibTeX
Citations
表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
关闭全屏
  • BibTeX
  • EndNote
  • RefWorks
  • TxT