Turbulent Flow Simulations of the Common Research Model Using Immersed Boundary Method

• 資料種別: 記事
• タイトル: Turbulent Flow Simulations of the Common Research Model Using Immersed Boundary Method
• 著者標目: Yoshiharu Tamaki; Taro Imamura
• 出版年月日等: 2018-06
• 出版年（W3CDTF）: 2018-06
• タイトル（掲載誌）: AIAA Journal
• 巻号年月日等（掲載誌）: 56 6
• 掲載巻: 56
• 掲載号: 6
• 掲載ページ: 2271-2282
• 掲載年月日（W3CDTF）: 2018-06
• ISSN（掲載誌）: 00011452
• 出版事項（掲載誌）: American Institute of Aeronautics and Astronautics (AIAA)
• 対象利用者: 一般
• DOI: 10.2514/1.j056654; https://doi.org/10.2514/1.j056654
• 作成日（W3CDTF）: 2018-04-03
• 関連情報（URI）: https://arc.aiaa.org/doi/pdf/10.2514/1.J056654
• 参照: Multifidelity Aeroelastic Model for Corrugated Morphing Structures; https://cir.nii.ac.jp/crid/1360017282467285376; UTCartによる民間航空機巡航形態の実機レイノルズ数定常流れ場解析; https://cir.nii.ac.jp/crid/1390859293124313216
• 参照: Green-Gauss/Weighted-Least-Squares Hybrid Gradient Reconstruction for Arbitrary Polyhedra Unstructured Grids; https://cir.nii.ac.jp/crid/1050003824960768896; Efficient dimension-by-dimension higher order finite-volume methods for a Cartesian grid with cell-based refinement; https://cir.nii.ac.jp/crid/1360004232075062144; Progress Towards a Cartesian Cut-Cell Method for Viscous Compressible Flow; https://cir.nii.ac.jp/crid/1360011143677917056; Simple and Robust Cut-Cell Method for High-Reynolds-Number-Flow Simulation on Cartesian Grids; https://cir.nii.ac.jp/crid/1360285714023106688; Near-wall modification of Spalart-Allmaras Turbulence Model for Immersed Boundary Method; https://cir.nii.ac.jp/crid/1360292618785749760; Drag Prediction for the NASA CRM Wing-Body-Tail Using CFL3D and OVERFLOW on an Overset Mesh; https://cir.nii.ac.jp/crid/1360292619316691328; The design and application of upwind schemes on unstructured meshes; https://cir.nii.ac.jp/crid/1360292619567922816; Strategies for turbulence modelling and simulations; https://cir.nii.ac.jp/crid/1360292619812112640; A strictly conservative Cartesian cut-cell method for compressible viscous flows on adaptive grids; https://cir.nii.ac.jp/crid/1360292620735110784; Parameter-Free Simple Low-Dissipation AUSM-Family Scheme for All Speeds; https://cir.nii.ac.jp/crid/1360574095337222144; Approximate Riemann solvers, parameter vectors, and difference schemes; https://cir.nii.ac.jp/crid/1360855569268071552; Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations; https://cir.nii.ac.jp/crid/1361137045761407616; Turbulent Wall Model for Immersed Boundary Methods; https://cir.nii.ac.jp/crid/1361137045962744832; On the suitability of the immersed boundary method for the simulation of high-Reynolds-number separated turbulent flows; https://cir.nii.ac.jp/crid/1361137046052439552; An immersed boundary method for compressible flows using local grid refinement; https://cir.nii.ac.jp/crid/1361418518779393920; Automatic Hexahedra Grid Generation Method for Component-Based Surface Geometry; https://cir.nii.ac.jp/crid/1361418518874775296; A Quadtree-based adaptive Cartesian/Quad grid flow solver for Navier-Stokes equations; https://cir.nii.ac.jp/crid/1361418521059298560; Application of the FUN3D Solver to the 4th AIAA Drag Prediction Workshop; https://cir.nii.ac.jp/crid/1361418521287647872; Toward the Fastest Unstructured CFD Code 'FaSTAR'; https://cir.nii.ac.jp/crid/1361981470674075520; Effect of a Nonlinear Constitutive Relation for Turbulence Modeling on Predicting Flow Separation at Wing-Body Juncture of Transonic Commercial Aircraft; https://cir.nii.ac.jp/crid/1362544418799824128; A hybrid Cartesian grid and gridless method for compressible flows; https://cir.nii.ac.jp/crid/1362825893725392768; A Level Set Approach for Computing Solutions to Incompressible Two-Phase Flow; https://cir.nii.ac.jp/crid/1363107369470496256; Exa PowerFLOW Simulations for the Sixth AIAA Drag Prediction Workshop; https://cir.nii.ac.jp/crid/1363388844591270528; Development of a Common Research Model for Applied CFD Validation Studies; https://cir.nii.ac.jp/crid/1363670320223332864; IMMERSED BOUNDARY METHODS; https://cir.nii.ac.jp/crid/1363670320247951488; DPW-5 Analysis of the CRM in a Wing-Body Configuration Using Structured and Unstructured Meshes; https://cir.nii.ac.jp/crid/1363670320347651456; A one-equation turbulence model for aerodynamic flows; https://cir.nii.ac.jp/crid/1363951794360241024
• 連携機関・データベース: 国立情報学研究所 : CiNii Research; https://cir.nii.ac.jp/
• 提供元機関・データベース: Crossref; https://www.crossref.org; 科学研究費助成事業データベース; https://kaken.nii.ac.jp/ja

• 要約等: Transonic turbulent flows around the NASA Common Research Model are simulated to investigate the capability of the Cartesian-grid-based flow solver UT...