@inproceedings{oai:jaxa.repo.nii.ac.jp:00046350,
 author = {北村, 圭一 and 小川, 優 and 瀧本, 浩之 and 金森, 正史 and 橋本, 敦 and Kitamura, Keiichi and Ogawa, Suguru and Takimoto, Hiroyuki and Kanamori, Masashi and Hashimoto, Atsushi},
 book = {宇宙航空研究開発機構特別資料: 第51回流体力学講演会/第37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 51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium},
 month = {Feb},
 note = {第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム (2019年7月1日-3日. 早稲田大学早稲田キャンパス国際会議場), 新宿区, 東京, 51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium (July 1-3, 2019. International Conference Center, Waseda University), Shinjuku-ku, Tokyo, Japan, The Delayed Detached-Eddy-Simulation [Spalart et al., Theor. Comput. Fluid Dyn. 2006] has been improved [coined as “HR (High-Resolution)-DDES”], and applied to an unsteady turbulence simulation of a low speed buffet around a whole aircraft (NASA Common Research Model). The HR-DDES is not a single turbulence model. It is instead a framework comprised of DDES with calibrated turbulence model coefficients and improved LES (Large-Eddy-Simulation) / RANS (Reynolds-Averaged-Navier-Stokes) transition. As a result, the pressure distributions over the main wing are dramatically improved especially at 13.1% cross-section from the center-plane. The HR-DDES serves as a good alternative to the conventional counterpart for practitioners/users/aeronautical engineers without major coding or code modifications., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1930011009, レポート番号: JAXA-SP-19-007},
 pages = {125--134},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {高解像度DDESによる低速バフェット解析},
 volume = {JAXA-SP-19-007},
 year = {2020}
}