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Multiblock Grid Generation: Results of the EC/Brite-Euram Project Euromesh, 1990

Description: Multiblock Grid Generation: Results of the EC/Brite-Euram Project Euromesh, 1990 1992 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 1970s. 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 1990s: 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. FORMAT Paperback LANGUAGE English CONDITION Brand New Publisher Description 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 1970s. 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 1990s: 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. Table of Contents 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. Long Description 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 1970s. 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 1990s: 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. Details ISBN3528076445 Short Title MULTIBLOCK GRID GENERATION 199 Publisher Vieweg+teubner Verlag Edition Description 1993 Series Notes on Numerical Fluid Mechanics and Multidisciplinary Des Language English ISBN-10 3528076445 ISBN-13 9783528076443 Media Book Format Paperback Series Number 44 Illustrations Yes Edition 93199th Subtitle Results of the EC/BRITE-EURAM Project EUROMESH, 1990-1992 Pages 331 DEWEY 518 Year 1993 Imprint Friedrich Vieweg & Sohn Verlagsgesellschaft mbH Place of Publication Wiesbaden Country of Publication Germany Edited by D.A. King Birth 1939 Publication Date 1993-01-01 DOI 10.1604/9783528076443;10.1007/978-3-322-87881-6 Audience Professional and Scholarly We've got this At The Nile, if you're looking for it, we've got it. With fast shipping, low prices, friendly service and well over a million items - you're bound to find what you want, at a price you'll love! TheNile_Item_ID:96318364;

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Multiblock Grid Generation: Results of the EC/Brite-Euram Project Euromesh, 1990

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ISBN-13: 9783528076443

Book Title: Multiblock Grid Generation: Results of the EC/Brite-Euram Project

Number of Pages: 331 Pages

Language: English

Publication Name: Multiblock Grid Generation: Results of the Ec/Brite-Euram Project Euromesh, 1990-1992

Publisher: Friedrich Vieweg & Sohn Verlagsgesellschaft Mbh

Publication Year: 1993

Subject: Mathematics

Item Height: 235 mm

Item Weight: 522 g

Type: Textbook

Author: Nigel P. Weatherill

Subject Area: Mechanical Engineering

Item Width: 155 mm

Format: Paperback

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