摘要
本文提出了一种确定叶片标准化载荷分布的方法,并结合文献中的反问题设计方法,对已有叶型进行了模化设计,经过三维几何造型及气动分析,给出了比较合理的设计结果。
A method of normalized blade loading determination is presented in this paper.By referencing an inverse cascade design method found in reference,two stages of gas turbine blades has been modelling from another gas turbine.Three-dimensional aerodynamics analysis of the two stages is presented here,the results are quite reasonable.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
2014年第5期862-866,共5页
Journal of Engineering Thermophysics