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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Библиографические подробности
Главные авторы: Ng Eddie Yin-Kwee, Liu Ningyu, Lim Hong Ngiap, Tan Daniel
Формат: Artigo
Язык:Inglês
Опубликовано: Hindawi Limited 2005-01-01
Серии:International Journal of Rotating Machinery
Предметы:
improved integral method
inlet distortion propagation
axial-flow compressor
airfoil characteristics
Online-ссылка:http://www.hindawi.net/access/get.aspx?journal=ijrm&volume=2005&pii=S1023621X03503025
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