A closed advancing-layer method with connectivity optimization-based mesh movement for viscous mesh generation
- 242 Downloads
- 2 Citations
Abstract
A new closed advancing-layer method for generating high-aspect-ratio elements in the boundary-layer (BL) region is presented. This approach utilizes a recent connectivity optimization-based moving mesh strategy for deforming the volume mesh as the BL is inflated. It handles very efficiently BL front collision and produces a natural smooth anisotropic blending between colliding layers. Moreover, it provides a robust strategy to couple unstructured anisotropic mesh adaptation and high-aspect-ratio elements pseudo-structured BL meshes. The proposed method is directly compared to a well-established open advancing-layer method. Results for typical aerospace configurations are presented that provide a clear comparison between both methods as well as the effectiveness of the connectivity optimization-based moving mesh strategy. They show that the closed method yields similar results in terms of mesh quality and efficiency, and that the considered moving mesh strategy is an efficient and effective method for deforming the unstructured volume mesh.
Keywords
Unstructured mesh generation Advancing-layer Boundary-layer mesh Viscous grid Moving meshReferences
- 1.Alauzet F (2012) Contributions aux méthodes numériques pour l’adaptation de maillage et le maillage mobile. Université Pierre et Marie Curie, Paris VI, Paris, France, Habilitation à Diriger des RecherchesGoogle Scholar
- 2.Alauzet F (2014) A changing-topology moving mesh technique for large displacement. Eng Comp 30(2):175–200CrossRefGoogle Scholar
- 3.Alauzet F, Loseille A (2010) High order sonic boom modeling by adaptive methods. J Comput Phys 229:561–593MATHMathSciNetCrossRefGoogle Scholar
- 4.Alauzet F, Mehrenberger M (2010) P1-conservative solution interpolation on unstructured triangular meshes. Int J Numer Meth Eng 84(13):1552–1588MATHMathSciNetCrossRefGoogle Scholar
- 5.Aubry R, Löhner R (2009) Generation of viscous grids at ridges and corners. Int J Numer Meth Eng 77:1247–1289MATHCrossRefGoogle Scholar
- 6.Baker T, Cavallo P (1999) Dynamic adaptation for deforming tetrahedral meshes. AIAA J 19:2699–3253Google Scholar
- 7.Bottasso C, Detomi D (2002) A procedure for tetrahedral boundary layer mesh generation. Eng Comput 18:66–79MATHCrossRefGoogle Scholar
- 8.Dobrzynski C, Frey P (2008) Anisotropic Delaunay mesh adaptation for unsteady simulations. In: Proceedings of the 17th international meshing roundtable, pp. 177–194. Springer, BerlinGoogle Scholar
- 9.Frey P, Alauzet F (2005) Anisotropic mesh adaptation for CFD computations. Comput Methods Appl Mech Eng 194(48–49):5068–5082MATHMathSciNetCrossRefGoogle Scholar
- 10.Frey P, George P (2008) Mesh generation. In: Application to finite elements, 2nd edn. ISTE Ltd, Wiley, New YorkGoogle Scholar
- 11.Garimella R, Shephard M (2000) Boundary layer mesh generation fro viscous flow simulations. Int J Numer Meth Fluids 49:193–218MATHCrossRefGoogle Scholar
- 12.George P, Hecht F, Saltel E (1991) Automatic mesh generator with specified boundary. Comput Methods Appl Mech Eng 92:269–288MATHMathSciNetCrossRefGoogle Scholar
- 13.Hassan O, Morgan K, Probert E, Peraire J (1996) Unstructured tetrahedral mesh generation for three-dimensional viscous flows. Int J Numer Meth Eng 39:549–567MATHCrossRefGoogle Scholar
- 14.Ito Y, Nakahashi, K (2002) Unstructured mesh generation for viscous flow computations. In: Proceedings of the 11th international meshing roundtable, pp 367–377Google Scholar
- 15.Löhner R (1999) Generation of unstructured grids suitable for RANS calculations. In: 37th AIAA aerospace sciences meetingGoogle Scholar
- 16.Löhner R, Parikh P (1988) Three-dimensional grid generation by the advancing front method. Int J Numer Meth Fluids 9:1135–1149CrossRefGoogle Scholar
- 17.Loseille A, Dervieux A, Alauzet F (2010) Fully anisotropic goal-oriented mesh adaptation for 3D steady Euler equations. J Comput Phys 229:2866–2897MATHMathSciNetCrossRefGoogle Scholar
- 18.Loseille A, Löhner R (2010) Adaptive anisotropic simulations in aerodynamics. In: 48th AIAA aerospace sciences meeting. AIAA Paper 2010-169, Orlando, FLGoogle Scholar
- 19.Loseille A, Löhner R (2011) Boundary layer mesh generation and adaptivity. In: 49th AIAA aerospace sciences meeting. AIAA Paper 2011-894, Orlando, FLGoogle Scholar
- 20.Marcum D (1995) Generation of unstructured grids for viscous flow applications. In: 33th AIAA aerospace sciences meetingGoogle Scholar
- 21.Marcum D (1996) Adaptive unstructured grid generation for viscous flow applications. AIAA J 34(8):2440–2443MATHCrossRefGoogle Scholar
- 22.Marcum D (1998) Unstructured grid generation using automatic point insertion and local reconnection. In: Thompson JF, Soni B, Weatherill NP (eds) The handbook of grid generation, chap 18, pp 1–31. CRC Press, New YorkGoogle Scholar
- 23.Marcum D, Alauzet F (2013) Unstructured mesh generation using advancing layers and metric-based transition. In: 21th AIAA computational fluid dynamics conference., AIAA PaperSan Diego, CA, USA, pp 2013–2710Google Scholar
- 24.Marcum D, Alauzet F, Marechal L (2011) Bloom: a closed advancing-layer boundary-layer mesh generator. Internal report, INRIAGoogle Scholar
- 25.Marcum D, Weatherill N (1995) Unstructured grid generation using iterative point insertion and local reconnection. AIAA J 33(9):1619–1625MATHCrossRefGoogle Scholar
- 26.Pirzadeh S (1994) Viscous unstructured three dimensional grids by the advancing-layers method. In: 32th AIAA aerospace sciences meetingGoogle Scholar
- 27.Sharov D, Nakahashi K (1998) Hybrid prismatic/tetrahedral grid generation for viscous flow applications. AIAA J 36(2):157–162MATHCrossRefGoogle Scholar
- 28.Yang Z, Mavriplis D (2007) Higher-order time integration schemes for aeroelastic applications on unstructured meshes. AIAA J 45(1):138–150CrossRefGoogle Scholar