Multiblock grid generation : results of the EC/BRITE-EURAM project EUROMESH, 1990-1992
著者
書誌事項
Multiblock grid generation : results of the EC/BRITE-EURAM project EUROMESH, 1990-1992
(Notes on numerical fluid mechanics, v. 44)
Vieweg, c1993
- タイトル別名
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Report on community research in aeronautics
大学図書館所蔵 全12件
  青森
  岩手
  宮城
  秋田
  山形
  福島
  茨城
  栃木
  群馬
  埼玉
  千葉
  東京
  神奈川
  新潟
  富山
  石川
  福井
  山梨
  長野
  岐阜
  静岡
  愛知
  三重
  滋賀
  京都
  大阪
  兵庫
  奈良
  和歌山
  鳥取
  島根
  岡山
  広島
  山口
  徳島
  香川
  愛媛
  高知
  福岡
  佐賀
  長崎
  熊本
  大分
  宮崎
  鹿児島
  沖縄
  韓国
  中国
  タイ
  イギリス
  ドイツ
  スイス
  フランス
  ベルギー
  オランダ
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  アメリカ
内容説明・目次
内容説明
Computational Fluid Dynamics research, especially for aeronautics, continues to be a rewarding and industrially relevant field of applied science in which to work. An enthusiastic international community of expert CFD workers continue to push forward the frontiers of knowledge in increasing number. Applications of CFD technology in many other sectors of industry are being successfully tackled. The aerospace industry has made significant investments and enjoys considerable benefits from the application of CFD to its products for the last two decades. This era began with the pioneering work ofMurman and others that took us into the transonic (potential flow) regime for the first time in the early 1970's. We have also seen momentous developments of the digital computer in this period into vector and parallel supercomputing. Very significant advances in all aspects of the methodology have been made to the point where we are on the threshold of calculating solutions for the Reynolds-averaged Navier-Stokes equations for complete aircraft configurations. However, significant problems and challenges remain in the areas of physical modelling, numerics and computing technology. The long term industrial requirements are captured in the U. S. Governments 'Grand Challenge' for 'Aerospace Vehicle Design' for the 1990's: 'Massively parallel computing systems and advanced parallel software technology and algorithms will enable the development and validation of multidisciplinary, coupled methods. These methods will allow the numerical simulation and design optimisation of complete aerospace vehicle systems throughout the flight envelope'.
目次
I. Introduction.- The EUROMESH Project.- An introduction to grid generation using the multiblock approach.- II. Topology Generation.- Topology generation within CAD systems.- A topological modeller.- Advancing front technique used to generate block quadrilaterals.- III. Surface Grid Generation and Geometry Modelling.- Surface mesh generation using projections.- Generation of surface grids using elliptic PDEs.- Generation of structured meshes over complex surfaces.- Surface modelling using Coons multipatch and non-uniform rational surface.- Reparametrization of block boundary surface grids.- Aircraft surface generation.- IV. Volume Grid Generation.- Use of ONERA grid optimization method at CASA.- Multi-block mesh generation for complete aircraft configurations.- Development of 3D multi-block mesh generation tools.- Multi-block mesh optimization.- Smoothing of grid discontinuities across block boundaries.- V. Grid Optimization and Adaption Methods.- Grid adaption in computational aerodynamics.- Embedding within structured multi-block computational fluid dynamics simulation.- Adaptive mesh generation within a 2D CFD environment using optimization techniques.- Two dimensional multi-block grid optimisation by variational techniques.- Local mesh enrichment for a block structured 3D Euler solver.- The adaptation of two-dimensional multiblock structured grids using a PDE-based method.- Contribution to the development of a multiblock grid optimization and adaption code.- General grid adaptivity for flow simulation.- Error estimates and mesh adaption for a cell vertex finite volume scheme.- Multigrid methods for the acceleration and the adaptation of the transonic flow problems.
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