压气机进口周期性动态畸变的实验研究
EXPERIMENTAL RESEARCH ON THE RESPONSE OF AN AXIAL COMPRESSOR TO INLET PERIODIC DYNAMIC DISTORTION作者机构:南京航空学院
出 版 物:《航空动力学报》 (Journal of Aerospace Power)
年 卷 期:1990年第5卷第1期
页 面:74-75页
核心收录:
学科分类:082502[工学-航空宇航推进理论与工程] 08[工学] 0825[工学-航空宇航科学与技术]
摘 要:A pitot pressure pulsation generator and a data acquisition and processing system have been built up for this *** response of a low pressure compressor to two kinds of inlet dynamic flow modes (axisymmetric or distorted) are investigated under the conditions of the compressor with or without a *** results show that there is a sensitive frequency at which the perturbation is amplified through the *** sensitive frequency is influenced not by inlet distortion,but by the plenum in the present research.