摘要
本文应用时间相关法进行了径向透平可转导叶二维跨音无粘流场的数值计算,应用动量积分关系式解法进行了边界层计算并得到有关的气动性能参数。
A numerical solution based on tine dependent method is applied for Solving two dimensional invisicid flows around radial turbine guide vanes. Computations of the boundary layers then conducted by Head's method and the aerodynamical performance parameters are obtained.
出处
《上海工程技术大学学报》
CAS
1994年第3期11-14,共4页
Journal of Shanghai University of Engineering Science
