@inproceedings{oai:jaxa.repo.nii.ac.jp:00005639,
 author = {堤, 誠司 and 河合, 宗司 and 高木, 亮治 and 藤井, 孝藏 and 有田, 誠 and Tsutsumi, Seiji and Kawai, Soshi and Takaki, Ryoji and Fujii, Kozo and Arita, Makoto},
 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 = {The generation and propagation of pressure waves from H-2A launch vehicle are analyzed numerically. The Mach wave radiated from a wavy shear-layer of exhaust plumes is revealed to be the dominant noise source. The Mach wave is reflected by the constructions of the launch-pad, then, propagates to the vehicles, causing the acoustic loads. It also turns out that the acoustic loads due to the Mach wave shows local maximum value with the ascent of the launch vehicle., 資料番号: AA0063742033, レポート番号: JAXA-SP-07-016},
 pages = {202--207},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {H-2Aロケット打上げ時に排気プルームから生じる圧力波の発生/伝播に関する研究},
 volume = {JAXA-SP-07-016},
 year = {2008}
}