@inproceedings{oai:jaxa.repo.nii.ac.jp:00002946,
 author = {高橋, 良尚 and 松島, 紀佐 and 清水, 亮介 and Takahashi, Yoshinao and Matsushima, Kisa and Shimizu, Ryosuke},
 book = {宇宙航空研究開発機構特別資料: 第50回流体力学講演会/第36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 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium},
 month = {Feb},
 note = {第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎, 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan, This article investigates effect of mesh distribution in wakes and distant flow-fields from an airplane on resulted flow phenomena when performing RANS CFD simulation. Heretofore, mesh distribution in those flow-fields is rather coarse. It is not sufficient for grasping accurate wake phenomena which are important for obtaining aerodynamic coefficient by wake integration as well as evaluating wake turbulence effect on others. The investigation is conducted regarding three subjects. The first one is mesh distribution in the vicinity of far-field boundaries of a computational domain. The second is to enlarge a computational domain, while the other is mesh distribution on downstream field of airplane. Through the investigation, several useful clues have been obtained for attaining good flow resolution in those fields by CFD., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1830029017, レポート番号: JAXA-SP-18-005},
 pages = {153--158},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {CFD 解析における物体後流域や遠方境界のメッシュの影響},
 volume = {JAXA-SP-18-005},
 year = {2019}
}