@inproceedings{oai:jaxa.repo.nii.ac.jp:00003495,
 author = {三坂, 孝志 and 鵜飼, 孝博 and 小西, 康郁 and 大林, 茂 and Misaka, Takashi and Ukai, Takahiro and Konishi, Yasufumi and Obayashi, Shigeru},
 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, This study numerically investigated an adaptive mesh refinement method based on experimental measurement. The difference of experimental and numerical results was propagated by an adjoint model of the radial basis function-based reduced-order model (RBF-ROM), which was derived from snapshots of a preceding numerical simulation. The incompressible Navier-Stokes equations were solved on the framework of the building cube method (BCM) for generating the snapshots and the mesh refinement was realized by utilizing the data structure of the BCM, i.e., a BCM mesh was refined by dividing cubes. The error of the numerical simulation was evaluated by two CFD runs with different mesh resolutions and the region of mesh refinement was defined by the inner product of the error and the measurement sensitivity obtained from the adjoint model of the RBF-ROM. By considering the measurement sensitivity, the difference of meshes after refinement appeared near the object, i.e., the region of mesh refinement was focused on the wake where the pseudo measurement was carried out., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630031020, レポート番号: JAXA-SP-16-007},
 pages = {157--160},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {計測データに基づく格子細分化手法},
 volume = {JAXA-SP-16-007},
 year = {2016}
}