@inproceedings{oai:jaxa.repo.nii.ac.jp:00005623,
 author = {岩永, 則城 and 金田, 英和 and 村上, 桂一 and 北村, 圭一 and 橋本, 敦 and 青山, 剛史 and 中村, 佳朗 and Iwanaga, Noriki and Kaneda, Hidekazu and Murakami, Keiichi and Kitamura, Keiichi and Hashimoto, Atsushi and Aoyama, Takashi and Nakamura, Yoshiaki},
 book = {宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集, JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007},
 month = {Feb},
 note = {Acoustic loads are the principal source of structural vibration and internal noise during launch or static-firing operations. The loads cause various problems, so it is important to predict the acoustic loads on space vehicles such as a rocket. Conventionally, the prediction has been made by empirical methods. These methods have some limitations, since shielding and reflection are difficult to be dealt with. To avoid these difficulties, we are planning to use our LEE (Linearized Euler Equation) code and evaluate the acoustic field to predict the acoustic loads on a rocket. As a first step, we report the results of some benchmark tests for validating our code's precision., 資料番号: AA0063742017, レポート番号: JAXA-SP-07-016},
 pages = {107--112},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {LEEによるロケットの音響効果予測},
 volume = {JAXA-SP-07-016},
 year = {2008}
}