The aerodynamic design of a radialturbine is described in this paper.
主要进行了某向心透平的气动设计。
2
An expression for the efficiency of the wheel periphery of the radialturbine and a discussion of the concept of the degree of reaction of the radial impulse stage are given.
文中推导了径流式透平的轮周效率表达式，阐述了径流式透平冲动式级的概念。
3
An efficient model based on radial basis function neural network and intelligent estimating method for data fusion of the turbine-generator is presented.