@inproceedings{oai:jaxa.repo.nii.ac.jp:00004709,
 author = {佐々木, 大輔 and 恩田, 博 and 石田, 崇 and 中橋, 和博 and 高橋, 俊 and Sasaki, Daisuke and Onda, Hiroshi and Ishida, Takashi and Nakahashi, Kazuhiro and Takahashi, Shun},
 book = {宇宙航空研究開発機構特別資料: 第42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2010 論文集, JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010},
 month = {Feb},
 note = {第42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2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP), 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25,  2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan, Landing gear is one of critical noise sources at landing, thus it is expected to develop CFD and CAA solvers to estimate the aerodynamic noise. In this study, block-structured Cartesian-based CFD solver, Building-Cube Method, is applied to predict the flowfield around the JAXA Landing gear Evaluation Geometry model. The capability of three-dimensional unsteady incompressible flow solver for a landing gear has been demonstrated through simple and complicated landing gear models., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967002, レポート番号: JAXA-SP-10-012},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Building-Cube 法によるJAXA主脚騒音模型の非定常流体解析},
 volume = {JAXA-SP-10-012},
 year = {2011}
}