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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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| 主要な著者: | , , , |
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| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
Hindawi Limited
2005-01-01
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| シリーズ: | International Journal of Rotating Machinery |
| 主題: | |
| オンライン･アクセス: | http://www.hindawi.net/access/get.aspx?journal=ijrm&volume=2005&pii=S1023621X03503025 |
| タグ: |
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