@inproceedings{oai:jaxa.repo.nii.ac.jp:00004395,
 author = {北村, 圭一 and 嶋, 英志 and Kitamura, Keiichi and Shima, Eiji},
 book = {宇宙航空研究開発機構特別資料: 第43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2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43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2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, The proposed method is a simple and parameter-free second slope limiter for unstructured grids, which is designed for use after any existing (first) limiters to stabilize the solution at subsonic speeds. The present second limiting is such that the first limiter is activated near the shock and supersonic regions, while turned off elsewhere in a very smooth manner, by using only lccal Mach number information. Numerical results demonstrated that the proposed second limiter retains the formal second-order accuracy, and also that it dramatically improved convergence at subsoniuc speeds on unstructured grids. In spite of these, the proposed formulation is simpler than exiting second limiters, with only 1 % additional cost requirement., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207023, レポート番号: JAXA-SP-11-015},
 pages = {137--142},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {非構造格子空カシミュレーションのための第2制限関数},
 volume = {JAXA-SP-11-015},
 year = {2012}
}