摘要
本文通过对几何参数已确定的平面叶栅实验结果的归纳与气动分析,给出进口马赫数M1很低时平面叶栅特性。为进一步分析压缩器作功增压与损失的关系,压缩器特性以及压缩器不稳定工作等问题打下必要的基础。
This thesis generalizes from the experiment result of the plane blading which is definitely geometry parameter,and the air operated analysis, and say that the characteristic of the plane blading when the imported Mach(M1) is lower. To lay the necessary foundation for analying the realation of compressor that it makes the merit Turbo-Charged and loss, the characteristic of compressor and it's abnormal work problems.
出处
《试验技术与试验机》
2007年第4期25-26,31,共3页
Test Technology and Testing Machine
关键词
气流转折角
损失系数
平面叶栅特性
shock angle
airflow-turning angle
loss coefficient
flane-vane feature