An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor
<p>An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics, with less assumptions needed for derivati...
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| Format: | Article |
| Language: | English |
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Wiley
2005-01-01
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| Series: | International Journal of Rotating Machinery |
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| Online Access: | http://www.hindawi.net/access/get.aspx?journal=ijrm&volume=2005&pii=S1023621X03503025 |
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| author | Ng Eddie Yin-Kwee Liu Ningyu Lim Hong Ngiap Tan Daniel |
| author_facet | Ng Eddie Yin-Kwee Liu Ningyu Lim Hong Ngiap Tan Daniel |
| author_sort | Ng Eddie Yin-Kwee |
| collection | DOAJ |
| description | <p>An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics, with less assumptions needed for derivation. The results indicate that the original integral method (Kim et al., 1996) underestimated the propagation of inlet flow distortion. The effects of inlet flow parameters on the propagation of inlet distortions as well as on the compressor performance and characteristic are simulated and analyzed. From the viewpoint of compressor efficiency, the propagation of inlet flow distortion is further described using a compressor critical performance and its associated critical characteristic. The results present a realistic physical insight to an axial-flow compressor behavior with a propagation of inlet distortion.</p> |
| format | Article |
| id | doaj-art-9bd38049d61e49dbbdd2b72d75e7dbd1 |
| institution | Kabale University |
| issn | 1023-621X |
| language | English |
| publishDate | 2005-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Rotating Machinery |
| spelling | doaj-art-9bd38049d61e49dbbdd2b72d75e7dbd12025-02-03T01:20:16ZengWileyInternational Journal of Rotating Machinery1023-621X2005-01-0120052117127An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial CompressorNg Eddie Yin-KweeLiu NingyuLim Hong NgiapTan Daniel<p>An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics, with less assumptions needed for derivation. The results indicate that the original integral method (Kim et al., 1996) underestimated the propagation of inlet flow distortion. The effects of inlet flow parameters on the propagation of inlet distortions as well as on the compressor performance and characteristic are simulated and analyzed. From the viewpoint of compressor efficiency, the propagation of inlet flow distortion is further described using a compressor critical performance and its associated critical characteristic. The results present a realistic physical insight to an axial-flow compressor behavior with a propagation of inlet distortion.</p>http://www.hindawi.net/access/get.aspx?journal=ijrm&volume=2005&pii=S1023621X03503025improved integral methodinlet distortion propagationaxial-flow compressorairfoil characteristics |
| spellingShingle | Ng Eddie Yin-Kwee Liu Ningyu Lim Hong Ngiap Tan Daniel An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor International Journal of Rotating Machinery improved integral method inlet distortion propagation axial-flow compressor airfoil characteristics |
| title | An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor |
| title_full | An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor |
| title_fullStr | An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor |
| title_full_unstemmed | An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor |
| title_short | An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor |
| title_sort | improved integral method for prediction of distorted inlet flow propagation in axial compressor |
| topic | improved integral method inlet distortion propagation axial-flow compressor airfoil characteristics |
| url | http://www.hindawi.net/access/get.aspx?journal=ijrm&volume=2005&pii=S1023621X03503025 |
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