@inproceedings{oai:jaxa.repo.nii.ac.jp:00005930,
 author = {浦, 弘樹 and 伊藤, 健 and 横川, 譲 and Ura, Hiroki and Ito, Takeshi and Yokokawa, Yuzuru},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第37回・第38回, JAXA Special Publication: Proceedings of the 37th and 38th JAXA Workshops on Investigation and Control of Boundary-Layer Transition},
 month = {Feb},
 note = {Phased-Array Microphone system has been developed at 2 m x 2 m Low-speed Wind Tunnel (LWT2) of JAXA. As a function checkout of the system, NACA0012 airfoil was tested. The results of this test were observed distinctly the noise generated near or on the trailing edge. In this paper, the outline of the results is reported., 資料番号: AA0063156011, レポート番号: JAXA-SP-06-013},
 pages = {35--38},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Phased-ArrayによるNACA0012翼型のTEノイズに関する研究},
 volume = {JAXA-SP-06-013},
 year = {2007}
}