燃气轮机热力设计程序。包括低压压气机，高压压气机，燃烧室，高压涡轮，中压涡轮，低压涡轮在内的整个燃气轮机的热力设计。-Gas turbine thermal design process. Including the low-pressure compressor, high pressure compressor, combustor, high pressure turbine, an intermediate pressure turbine and low pressure turbin

20MW及以上的汽轮机低压进汽管的计算-20MW and above the low-pressure turbine inlet steam pipe calculation。。。。。。。。

Direct numerical simulations have been performed to study the flow around a high-lift turbine blade for low and high levels of turbulence intensity. Initially a two-dimensional simulation has been carried out to study the dominant two-dimensional ph

Results are presented of Bi Global stability analysis of incompressible flow over a row of T-106/300 Low Pressure Turbine blades. In particular the two- and three-dimensional stability of a two-dimensional steady state is investigated for Reynolds