@inproceedings{oai:jaxa.repo.nii.ac.jp:00006605,
 author = {金子, 宗嗣 and 中村, 佳朗 and 小池, 勝 and Kaneko, Munetsugu and Nakamura, Yoshiaki and Koike, Masaru},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {The aerodynamic sound generated from a protuberance has been simulated in this study. The protuberance, which is placed on a flat plate, has three kinds of shape at the leading edge. The propagation of sound waves is examined by solving the three-dimensional N-S equations to observe small pressure fluctuations both in the near and far fields. Numerical results show that vortices created from near the leading edge may make pressure waves, leading to acoustic waves. Moreover, FFT analysis shows that the frequency profile partly agrees with experimental data., 資料番号: AA0047427004, レポート番号: JAXA-SP-03-002},
 pages = {17--22},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {突起物から発生する空力音に対する丸みの影響},
 volume = {JAXA-SP-03-002},
 year = {2004}
}