@article{oai:jaxa.repo.nii.ac.jp:00032399,
 author = {谷田, 好通 and 長島, 利夫 and TANIDA, Y. and NAGASHIMA, T.},
 issue = {1_C},
 journal = {東京大学宇宙航空研究所報告},
 month = {Mar},
 note = {軸流ファンや圧縮機からの回転騒音の発生,伝播機構とその低減法,特に翼列の傾斜効果を明らかにする目的で計画された研究の内容が報告されている.新しく製作された回転翼列試験機の性能や測定系統の組立ての他に,翼列後流の減衰や音響特性に関する一連のデータが整理され,傾斜効果に関連して,3次元アクチュエータディスクの解析モデルが紹介されている., A new test rig has been built to investigate the discrete frequency sound generation from an axial fan or a compressor. Steady performance of the rig is found to be satisfactory at the design condition. Experimental particulars for the acoustic test are given and some of the test results are shown for both operation modes of a single rotor and/or the rotor plus stator cascades. One of the primary objectives in the present experiment is the effect of the blade tilting on the interaction between the blade cascades in relative motion, therefore an analytical model including this effect has been also proposed., 資料番号: SA0125620000},
 pages = {563--583},
 title = {<論文>軸流圧縮機からの回転騒音},
 volume = {14},
 year = {1978}
}