Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor
In order to detect the aerodynamic instability of a multistage axial compressor more accurately and earlier, the harmonic Fourier mean amplitude analysis method and heterotopic variance analysis method are developed. The dynamic instability prediction performance of the two methods is studied on a l...
Saved in:
Main Authors: | , , , , |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/8893792 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
_version_ | 1832560553530228736 |
---|---|
author | Baofeng Tu Xinyu Zhang Jun Hu Ming Zhong Bing Xiong |
author_facet | Baofeng Tu Xinyu Zhang Jun Hu Ming Zhong Bing Xiong |
author_sort | Baofeng Tu |
collection | DOAJ |
description | In order to detect the aerodynamic instability of a multistage axial compressor more accurately and earlier, the harmonic Fourier mean amplitude analysis method and heterotopic variance analysis method are developed. The dynamic instability prediction performance of the two methods is studied on a low-speed and a high-speed two-stage axial compressor. The harmonic Fourier mean amplitude analysis method is suitable for predicting the aerodynamic instability of a multistage axial compressor in the form of a rotating stall. Compared with the traditional harmonic Fourier analysis methods, the harmonic Fourier mean amplitude analysis method can capture the detail of the pressure signal more accurately and it can effectively prevent instability misjudgment. The heterotopic variance analysis method is developed based on the conventional variance analysis method, and it can be used to distinguish whether the compressor is in the rotating stall or the surge state. The heterotopic variance analysis method can predict the aerodynamic instability ahead of the harmonic Fourier mean amplitude analysis method, and fewer circumferential measuring points were employed. The layout of the measuring points also influences the detection of the aerodynamic instability of the compressor. The aerodynamic instability of the high-speed axial compressor can be predicted earlier by employing measuring points at the compressor outlet. |
format | Article |
id | doaj-art-c731d96e94784ef0ba5d7439259abdda |
institution | Kabale University |
issn | 1687-5966 1687-5974 |
language | English |
publishDate | 2021-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Aerospace Engineering |
spelling | doaj-art-c731d96e94784ef0ba5d7439259abdda2025-02-03T01:27:20ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742021-01-01202110.1155/2021/88937928893792Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial CompressorBaofeng Tu0Xinyu Zhang1Jun Hu2Ming Zhong3Bing Xiong4Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, ChinaJiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, ChinaJiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, ChinaSichuan Gas Turbine Research Establishment, Aero Engine Corporation of China, Mianyang, Sichuan 621700, ChinaSichuan Gas Turbine Research Establishment, Aero Engine Corporation of China, Mianyang, Sichuan 621700, ChinaIn order to detect the aerodynamic instability of a multistage axial compressor more accurately and earlier, the harmonic Fourier mean amplitude analysis method and heterotopic variance analysis method are developed. The dynamic instability prediction performance of the two methods is studied on a low-speed and a high-speed two-stage axial compressor. The harmonic Fourier mean amplitude analysis method is suitable for predicting the aerodynamic instability of a multistage axial compressor in the form of a rotating stall. Compared with the traditional harmonic Fourier analysis methods, the harmonic Fourier mean amplitude analysis method can capture the detail of the pressure signal more accurately and it can effectively prevent instability misjudgment. The heterotopic variance analysis method is developed based on the conventional variance analysis method, and it can be used to distinguish whether the compressor is in the rotating stall or the surge state. The heterotopic variance analysis method can predict the aerodynamic instability ahead of the harmonic Fourier mean amplitude analysis method, and fewer circumferential measuring points were employed. The layout of the measuring points also influences the detection of the aerodynamic instability of the compressor. The aerodynamic instability of the high-speed axial compressor can be predicted earlier by employing measuring points at the compressor outlet.http://dx.doi.org/10.1155/2021/8893792 |
spellingShingle | Baofeng Tu Xinyu Zhang Jun Hu Ming Zhong Bing Xiong Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor International Journal of Aerospace Engineering |
title | Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor |
title_full | Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor |
title_fullStr | Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor |
title_full_unstemmed | Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor |
title_short | Analysis Methods for Aerodynamic Instability Detection on a Multistage Axial Compressor |
title_sort | analysis methods for aerodynamic instability detection on a multistage axial compressor |
url | http://dx.doi.org/10.1155/2021/8893792 |
work_keys_str_mv | AT baofengtu analysismethodsforaerodynamicinstabilitydetectiononamultistageaxialcompressor AT xinyuzhang analysismethodsforaerodynamicinstabilitydetectiononamultistageaxialcompressor AT junhu analysismethodsforaerodynamicinstabilitydetectiononamultistageaxialcompressor AT mingzhong analysismethodsforaerodynamicinstabilitydetectiononamultistageaxialcompressor AT bingxiong analysismethodsforaerodynamicinstabilitydetectiononamultistageaxialcompressor |