@inproceedings{oai:jaxa.repo.nii.ac.jp:00003244,
 author = {松尾, 裕一 and 南部, 太介 and 溝渕, 泰寛 and 桑原, 匠史 and 桐原, 亮平 and 中森, 一郎 and Matsuo, Yuichi and Nambu, Taisuke and Mizobuchi, Yasuhiro and Kuwabara, Takuhito and Kirihara, Ryohei and Nakamori, Ichiro},
 book = {宇宙航空研究開発機構特別資料: 第49回流体力学講演会/第35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 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium},
 month = {Dec},
 note = {第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-40日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京, 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan, This paper describes the application of an adaptive mesh refinement method based on the block-based adaptation to the analysis of flow inside an engine cylinder. The suitability of the present AMR methodology, particularly of the time integration method and the effect of AMR to the computational results is shown. By comparing the results obtained using 1mm uniform mesh, 0.5mm uniform mesh, AMR mesh, we find the present block-based AMR method is effective for the high resolution of the flow analysis in the engine cylinder., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1730011010, レポート番号: JAXA-SP-17-004},
 pages = {79--82},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {エンジン筒内流動解析における格子細分化法の適用},
 volume = {JAXA-SP-17-004},
 year = {2017}
}