Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)
Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)
Numerical Simulation Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)
Research Center of Computational Mechanics, Inc.(RCCM)
Nagoya University
Institute of Fluid Science, Tohoku University
Institute of Fluid Science, Tohoku University
出版者
宇宙航空研究開発機構(JAXA)
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料
雑誌名(英)
JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012
44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan
抄録（英）
Several different sonic boom propagation analysis methods were applied for the D-SEND#1 test cases, and the results were validated by comparing to the measured data. The sonic boom signatures calculated by all of the methods were similar to the measured waveforms as a whole. However, some discrepancies were found in the detailed features of the signatures among the methods, especially the rise times in the shock structures.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
D-SEND#1 データを用いたソニックブーム伝播解析手法検証
61958016.pdf
(951.85KB)
