@article{oai:jaxa.repo.nii.ac.jp:00034569,
 author = {TANIDA, Yoshimichi and NAGASHIMA, Toshio},
 issue = {3},
 journal = {ISAS report/Institute of Space and Aeronautical Science,University of Tokyo},
 month = {Feb},
 note = {Nonuniformity of inlet flows through a test compressor stage has been studied based upon 3-D semi-actuator disk theory. The results show that the rotor blade vibration greatly influences the attenuation rate of distortion. The effects of the rotor/stator separation, the circumferential modal index and the tilting of the inlet distortion, are also demonstrated., 資料番号: SA2401428000},
 pages = {93--103},
 title = {Inlet Distortion and Blade Vibration in Turbomachines},
 volume = {46},
 year = {1981}
}