000 06047nam a22005895i 4500
001 978-3-642-03707-8
003 DE-He213
005 20140220084525.0
007 cr nn 008mamaa
008 100918s2010 gw | s |||| 0|eng d
020 _a9783642037078
_9978-3-642-03707-8
024 7 _a10.1007/978-3-642-03707-8
_2doi
050 4 _aTA357-359
072 7 _aTGMF
_2bicssc
072 7 _aTGMF1
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aSCI085000
_2bisacsh
082 0 4 _a620.1064
_223
100 1 _aKroll, Norbert.
_eeditor.
245 1 0 _aADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications
_h[electronic resource] :
_bResults of a collaborative research project funded by the European Union, 2006-2009 /
_cedited by Norbert Kroll, Heribert Bieler, Herman Deconinck, Vincent Couaillier, Harmen Ven, Kaare Sørensen.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c2010.
300 _aXIV, 498 p.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1612-2909 ;
_v113
505 0 _aThe ADIGMA Project -- The ADIGMA Project -- Research Activities -- Exploiting Data Locality in the DGM Discretisation for Optimal Efficiency -- Very High-Order Accurate Discontinuous Galerkin Computation of Transonic Turbulent Flows on Aeronautical Configurations -- Incorporating a Discontinuous Galerkin Method into the Existing Vertex-Centered Edge-Based Finite Volume Solver Edge -- Explicit One-Step Discontinuous Galerkin Schemes for Unsteady Flow Simulations -- RKDG with WENO Type Limiters -- IPG Discretizations of the Compressible Navier-Stokes Equations -- Development of Discontinuous Galerkin Method for RANS Equations on Multibloc Hexahedral Meshes -- Construction of High-Order Non Upwind Distribution Schemes -- High Order Residual Distribution Schemes Based on Multidimensional Upwinding -- Higher-Order Stabilized Finite Elements in an Industrial Navier-Stokes Code -- A Third-Order Finite-Volume Residual-Based Scheme on Unstructured Grids -- Investigation of Issues Relating to Meshing for Higher-Order Discretizations -- Synthesis Report on Shock Capturing Strategies -- Implicit Strategy and Parallelization of a High Order Residual Distribution Scheme -- Hybrid Multigrid DG/FV Methods for Viscous Turbulent Flows -- Semi-implicit Time Discretization of the Discontinuous Galerkin Method for the Navier-Stokes Equations -- Multigrid Optimization for Space-Time Discontinuous Galerkin Discretizations of Advection Dominated Flows -- COOLFluiD – A Collaborative Simulation Environment for Research in Aerodynamics -- Robust and Efficient Implementation of Very High-Order Discontinuous Galerkin Methods in CFD -- Agglomeration Multigrid for the Vertex-Centered Dual Discontinuous Galerkin Method -- Higher–Order Aerodynamic Computations Using an Edge Based Finite Volume Scheme -- Dynamic Load Balancing for Parallelization of Adaptive Algorithms -- Error Estimation and Adaptive Mesh Refinement for Aerodynamic Flows -- Adjoint–Based Correction of Aerodynamic Coefficients on Structured Multiblock Grids -- Goal-Oriented Mesh Adaptation in an Industrial Stabilized Finite Element Navier-Stokes Code -- Application of Feature-Based Grid Adaptation to Helicopter Rotor Flow -- High–Order hp–Adaptive Discontinuous Galerkin Finite Element Methods for Compressible Fluid Flows -- Treatment of the Non-polygonal Boundary with the Aid of NURBS -- HP-Adaption in Space-Time within an Explicit Discontinuous Galerkin Framework -- Anisotropic Mesh Adaptation in the Presence of Complex Boundaries -- Industrial Assessment of Newly Developed Technologies -- Requirements and Assessment Methodology -- Verification and Assessment -- Conclusion and Recommendations -- Conclusions and Recommendations.
520 _aThis volume contains results gained from the EU-funded 6th Framework project ADIGMA (Adaptive Higher-order Variational Methods for Aerodynamic Applications in Industry). The goal of ADIGMA was the development and utilization of innovative adaptive higher-order methods for the compressible flow equations enabling reliable, mesh independent numerical solutions for large-scale aerodynamic applications in aircraft industry. The ADIGMA consortium was comprised of 22 organizations which included the main European aircraft manufacturers, the major European research establishments and several universities, all with well proven expertise in Computational Fluid Dynamics (CFD). The book presents an introduction to the project, exhibits partners’ methods and ap-proaches and provides a critical assessment of the newly developed methods for industrial aerodynamic applications. The best numerical strategies for integration as major building blocks for the next generation of industrial flow solvers are identified.
650 0 _aEngineering.
650 0 _aEngineering mathematics.
650 0 _aHydraulic engineering.
650 0 _aAstronautics.
650 1 4 _aEngineering.
650 2 4 _aEngineering Fluid Dynamics.
650 2 4 _aAerospace Technology and Astronautics.
650 2 4 _aAppl.Mathematics/Computational Methods of Engineering.
650 2 4 _aNumerical and Computational Physics.
650 2 4 _aFluid- and Aerodynamics.
700 1 _aBieler, Heribert.
_eeditor.
700 1 _aDeconinck, Herman.
_eeditor.
700 1 _aCouaillier, Vincent.
_eeditor.
700 1 _aVen, Harmen.
_eeditor.
700 1 _aSørensen, Kaare.
_eeditor.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783642037061
830 0 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1612-2909 ;
_v113
856 4 0 _uhttp://dx.doi.org/10.1007/978-3-642-03707-8
912 _aZDB-2-ENG
999 _c111530
_d111530