@inproceedings{oai:jaxa.repo.nii.ac.jp:00003498,
 author = {安田, 章悟 and 菱田, 学 and 高木, 正英 and 南部, 太介 and 溝渕, 泰寛 and 松尾, 裕一 and Yasuda, Shogo and Hishida, Manabu and Takagi, Masahide and Nambu, Taisuke and Mizobuchi, Yasuhiro and Matsuo, Yuichi},
 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, A new flow solver using the compressible LES, Immersed Boundary method and Cartesian grid is developed for automotive internal combustion engine simulation. We incorporated the basic spray model in this solver and carried out parallel spray calculations. This paper presents the results of comparison of the calculation time between two parallel methods. One is particle process method that uses a dedicated process for particle calculation. The other is domain decomposition method in which a process assigned to each domain calculates spray and gas and communicates with other processes to send and receive particles which go outside and inside the domain. Under the condition in this study, we find that domain decomposition method is faster than particle process method., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630031023, レポート番号: JAXA-SP-16-007},
 pages = {173--176},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {境界埋め込み法を用いた等間隔直交格子ソルバにおけるDDM並列計算},
 volume = {JAXA-SP-16-007},
 year = {2016}
}