2   Artículos

 
en línea
Xiaobin Xu, Baojie Liu, Xianjun Yu and Guangfeng An    
The geometry of a compressor leading edge has an important effect on the aerodynamic performance at an off-designed incidence angle. The current geometric design methods of the leading edge are usually developed based on the flow characteristics at the d... ver más
Revista: Aerospace    Formato: Electrónico

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