摘要
本文主要是应用目前先进的Bzéier曲线曲面造型方法,发展了一种新型的叶片造型方法,用以满足在超声和跨声状况下对叶型进行灵活控制的需要。本文以某型轴流压气机级为例,进行了转、静叶造型和相应的计算分析,初步验证了该方法的可行性。
This paper studied a new technology of compressor blading using the state of the art Bézier curves and surfaces geometric model for a flexible control of the airfoil shape under the supersonic and transonic inlet condition. A compressor stage was selected to validate it＇s feasibility.
出处
《燃气涡轮试验与研究》
2008年第2期19-23,共5页
Gas Turbine Experiment and Research
