Design method for bionic turbine blade of aero-engine

The invention discloses an aero-engine bionic turbine blade design method which comprises the following steps: firstly, selecting a reference blade, and determining pressure surface data, suction surface data and mean camber line data of the reference blade at different spanwise position sections; i...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DUAN WENHUA, CHEN WEIJIE, XIANG KANGSHEN, LIAN JIANXIN, QIAO WEIYANG
Format: Patent
Sprache:chi ; eng
Schlagworte:
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