重庆理工大学学报（自然科学版）2016，Vol.30Issue(6)：64-69,6.DOI:10.3969/j.issn.1674-8425(z).2016.06.011
不同加载形式高负荷低压涡轮的性能分析
Performance Analysis of High Loaded Low Pressure Turbine with Different Loading Distribution
摘要
Abstract
The effect law of loading distribution on boundary layer development at wide range Reynolds number was studied through design three turbine blades with different load distribution but same load level.The research indicated that after-loaded airfoil is more sensitive to Reynolds number especially when at the low Reynolds numbers while the front and mid loaded airfoil is less sensitive. The research can provide theory guidance for the design of airfoil which worked at different work condition.关键词
负荷分布/雷诺数/边界层/气动损失Key words
load distribution/Reynolds number/boundary layer/aerodynamic loss分类
航空航天引用本文复制引用
白涛..不同加载形式高负荷低压涡轮的性能分析[J].重庆理工大学学报（自然科学版）,2016,30(6):64-69,6.基金项目
国家自然科学基金青年基金资助项目 （）
