Development of rotating linear cascade facility for simulating blade tip clearance flow 模拟叶尖间隙流的转动平面叶栅实验方案
3.
Abstract : a 3d numerical solution of transonic turbulent flowfield inside a compressor rotor is analyzed with a consideration of blade tip clearance 文摘:借助于考虑叶片顶部间隙的压气机转子内跨音速湍流流场的三维数值解,得到了该转子流场中的复杂涡系与波系结构。