Study on aerodynamic design of 1/2+1 counter-rotating compressor
It is of vital importance to develop counter-rotating compressor for military and national defense，and the aerodynamic design of counter-rotating compressors is a prerequisite for the purpose. A detailed analysis of the internal flow characteristics of the counter-rotating compressor is conducted，an...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-04-01
|
| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023142 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1850282728046460928 |
|---|---|
| author | LIU Jingyuan WU Tianyuan |
| author_facet | LIU Jingyuan WU Tianyuan |
| author_sort | LIU Jingyuan |
| collection | DOAJ |
| description | It is of vital importance to develop counter-rotating compressor for military and national defense，and the aerodynamic design of counter-rotating compressors is a prerequisite for the purpose. A detailed analysis of the internal flow characteristics of the counter-rotating compressor is conducted，and the aerodynamic design ideas and methods of the counter-rotating compressor are explored. On the basis of balancing the aerodynamic and geometric design parameters，as well as the coordination and matching between the front and rear rotor design parameters，a 1/2+1 counter-rotating compressor aerodynamic scheme design is completed and perform three-dimensional numerical verification. The results indicate that the coordination and matching of design parameters between the front and rear rotor blade rows，the values of design parameters of the rear rotor load coefficient and diffusion factor，as well as the elementary blade profile parameters of each blade row，have a significant impact on the performance of the compressor. The full three-dimensional numerical simulation results show that the designed counter-rotating compressor meets the overall performance indexes with high aerodynamic performance. |
| format | Article |
| id | doaj-art-b36ea54aaeac43708137431dff167a21 |
| institution | OA Journals |
| issn | 1674-8190 |
| language | zho |
| publishDate | 2025-04-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj-art-b36ea54aaeac43708137431dff167a212025-08-20T01:47:54ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902025-04-01162526110.16615/j.cnki.1674-8190.2025.02.0620250206Study on aerodynamic design of 1/2+1 counter-rotating compressorLIU Jingyuan0WU Tianyuan1School of Power and Energy, Nanchang Hangkong University, Nanchang 330063, ChinaSchool of Power and Energy, Nanchang Hangkong University, Nanchang 330063, ChinaIt is of vital importance to develop counter-rotating compressor for military and national defense，and the aerodynamic design of counter-rotating compressors is a prerequisite for the purpose. A detailed analysis of the internal flow characteristics of the counter-rotating compressor is conducted，and the aerodynamic design ideas and methods of the counter-rotating compressor are explored. On the basis of balancing the aerodynamic and geometric design parameters，as well as the coordination and matching between the front and rear rotor design parameters，a 1/2+1 counter-rotating compressor aerodynamic scheme design is completed and perform three-dimensional numerical verification. The results indicate that the coordination and matching of design parameters between the front and rear rotor blade rows，the values of design parameters of the rear rotor load coefficient and diffusion factor，as well as the elementary blade profile parameters of each blade row，have a significant impact on the performance of the compressor. The full three-dimensional numerical simulation results show that the designed counter-rotating compressor meets the overall performance indexes with high aerodynamic performance.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023142counter-rotating compressoraerodynamic designdesign criteriaaerodynamic performancenumerical simulation |
| spellingShingle | LIU Jingyuan WU Tianyuan Study on aerodynamic design of 1/2+1 counter-rotating compressor Hangkong gongcheng jinzhan counter-rotating compressor aerodynamic design design criteria aerodynamic performance numerical simulation |
| title | Study on aerodynamic design of 1/2+1 counter-rotating compressor |
| title_full | Study on aerodynamic design of 1/2+1 counter-rotating compressor |
| title_fullStr | Study on aerodynamic design of 1/2+1 counter-rotating compressor |
| title_full_unstemmed | Study on aerodynamic design of 1/2+1 counter-rotating compressor |
| title_short | Study on aerodynamic design of 1/2+1 counter-rotating compressor |
| title_sort | study on aerodynamic design of 1 2 1 counter rotating compressor |
| topic | counter-rotating compressor aerodynamic design design criteria aerodynamic performance numerical simulation |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023142 |
| work_keys_str_mv | AT liujingyuan studyonaerodynamicdesignof121counterrotatingcompressor AT wutianyuan studyonaerodynamicdesignof121counterrotatingcompressor |