@inproceedings{oai:jaxa.repo.nii.ac.jp:00003481,
 author = {金森, 正史 and 高橋, 孝 and 牧野, 好和 and 中, 右介 and 高橋, 英美 and 石川, 敬掲 and Kanamori, Masashi and Takahashi, Takashi and Makino, Yoshikazu and Naka, Yusuke and Takahashi, Hidemi and Ishikawa, Hiroaki},
 book = {宇宙航空研究開発機構特別資料: 第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium},
 month = {Dec},
 note = {第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川, 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan, Some numerical analyses results for predicting the effect of atmospheric turbulence on sonic boom, especially for the waveform observed in the D-SEND#2 flight test, are presented in this paper. The measured sonic boom in the flight test took the shape with a much gentler curve than the predicted one with no effect of atmospheric turbulence. Through some inspections of the flight test, it was found that the effect of atmospheric turbulence has possibility to give reasonable explanation on the deformation of waveform. This paper reports evidence on the latter possibility in detail through some steps: verification and validation by comparing with analytical solution or the result of other preceding researches., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630031006, レポート番号: JAXA-SP-16-007},
 pages = {69--78},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {D-SEND#2 飛行試験のソニックブームにおける大気乱流効果の数値解析},
 volume = {JAXA-SP-16-007},
 year = {2016}
}