Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University
Division of Advanced Mechanical Systems Engineering, Institute of Engineering, Tokyo University of Agriculture and Technology
JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010
巻
JAXA-SP-10-012
発行年
2011-02-28
会議概要（会議名, 開催地, 会期, 主催者等）
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)
会議概要（会議名, 開催地, 会期, 主催者等）（英）
42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan
抄録（英）
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.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Building-Cube 法によるJAXA主脚騒音模型の非定常流体解析
64967002.pdf
(1.56MB)
