By Norbert Kroll (auth.), Norbert Kroll, Heribert Bieler, Herman Deconinck, Vincent Couaillier, Harmen van der Ven, Kaare Sørensen (eds.)
This quantity includes effects received from the EU-funded sixth Framework undertaking ADIGMA (Adaptive Higher-order Variational equipment for Aerodynamic purposes in Industry). The target of ADIGMA used to be the improvement and usage of cutting edge adaptive higher-order tools for the compressible circulation equations allowing trustworthy, mesh self sufficient numerical recommendations for large-scale aerodynamic functions in airplane undefined. The ADIGMA consortium used to be constituted of 22 companies which incorporated the most eu plane brands, the key ecu learn institutions and a number of other universities, all with good confirmed services in Computational Fluid Dynamics (CFD). The booklet offers an creation to the undertaking, shows companions’ tools and ap-proaches and gives a severe evaluate of the newly constructed equipment for business aerodynamic functions. the simplest numerical innovations for integration as significant development blocks for the subsequent iteration of business stream solvers are pointed out.
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Extra info for ADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications: Results of a collaborative research project funded by the European Union, 2006-2009
Restrictions of the function Uh ∈ Vhd+2 onto Ti and T j are denoted Uhi and Uhj . Right: The boundary edge is the union of ∂ Tib and ∂ T jb , and the domain boundary outward unit normals are nˆ ib and nˆ jb . The domain boundary data, which is given by the boundary condition, is denoted uBC . -E. Ekstr¨om and M. Berggren A pseudo-code version of the algorithm can be found in the the article by Berggren et al. ; in essence, it is the same loops as for the FV code plus the volume integral of the DG scheme.
Gov/tsab/cfdlarc/aiaa-dpw/Workshop3/ 2. : Unified analysis of discontinuous Galerkin methods for elliptic problems. SIAM J. Numer. Anal. 39(5), 1749–1779 (2002) 3. 2–Investigation of Jacobian and Jacobian-free Newton-Krylov methods for implicit DG methods. de/as/adigma 4. : Discontinuous Galerkin solution of the Reynolds-averaged Navier-Stokes and k-ω turbulence model equations. Comput. & Fluids 34, 507–540 (2005) 5. : A high order discontinuous Galerkin method for compressible turbulent flows.
The discrepancy between the more accurate results on the two grids is still to be understood and no conclusion can be drawn about the asymptotic convergence of the two solutions. One issue could be the poor geometrical approximation of solid surfaces when using only quadratic mappings for the faces of very coarse meshes. Figure 8 shows how the pressure coefficient distribution of the P3 solution Fig. 12528 36 F. Bassi et al. Fig. 8 DLR-F6: pressure coefficient of P3 solution (◦ 1012360 DOFs) compared with TAU (—— 5102446 DOFs) and CFL3D (– – – 2256896 DOFs, – · – 7689088 DOFs, – ·· – 26224640 DOFs) on the coarse grid compares with reference results of the TAU and CFL3D codes taken from .
ADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications: Results of a collaborative research project funded by the European Union, 2006-2009 by Norbert Kroll (auth.), Norbert Kroll, Heribert Bieler, Herman Deconinck, Vincent Couaillier, Harmen van der Ven, Kaare Sørensen (eds.)