多级跨音速压气机S_2流面正反问题混合计算

MIXED CALCULATION OF DIRECT AND INVERSE PROBLEMS ALONG S_2 STREAM SURFACE IN MULTISTAGE TRANSONIC COMPRESSOR

多级跨音速压气机Ｓ＿２流面正反问题混合计算苏杰先，冯国泰，魏沫，胡昆（哈尔滨工业大学）一、前言大型航空发动机跨音速压气机的发展有力地促进了小型弹用发动机的飞速进步。美国的＂战斧＂式巡航导弹用发动机Ｆ１０７－ＷＲ－１００以及法国的弹用发动机ＴＲＩ－６０...

The predicted calculation has shown that bowed blades applied to stator of first stage in multistage transonic compressor can reduce endwall losses, leakage losses and shock losses.It can cause successive stages to improve its performance.