ARTICLE
Robust generation method of a signed distance function for preprocessing of cartesian-grid-based CFD
 
More details
Hide details
1
Faculty of Science and Engineering, Iwate University, Japan
 
 
Submission date: 2023-01-24
 
 
Final revision date: 2023-04-13
 
 
Acceptance date: 2023-04-18
 
 
Online publication date: 2023-05-31
 
 
Publication date: 2023-07-31
 
 
Corresponding author
Yuki Takeda   

Faculty of Science and Engineering, Iwate University, 4-3-5, Ueda, 020-8551, Morioka, Japan
 
 
Journal of Theoretical and Applied Mechanics 2023;61(3):453-463
 
KEYWORDS
TOPICS
ABSTRACT
In practical computational fluid dynamics simulations around industrial products with com- plex surface shapes, the robustness of preprocessing to “dirty” geometry is an important issue. The dirty STL (Standard Triangle Language) data contains errors such as gaps be- tween facets, overlapping of facets, and flipping of normal vectors. These errors in the STL data are difficult to avoid in 3D modeling of complex geometry. Using a Cartesian grid is advantageous to the boundary-fitted grid in the aspect of preprocessing for dirty STL files. In this study, a robust and automatic generation method of a signed distance function for the preprocessing of Cartesian grid solvers is proposed. To ensure robustness to the complex and dirty STL data, the proposed method uses information of all STL facets to determine each grid point. The proposed preprocessing method is verified by numerical simulation of the flow around the NASA common research model.
 
REFERENCES (16)
1.
Baerentzen J.A., Aanaes H., 2005, Signed distance computation using the angle weighted pseudonormal, IEEE Transactions on Visualization and Computer Graphics, 11, 3, 243-253.
 
2.
Carvalho P.C.P., Cavalcanti P.R., 1995, Point in Polyhedron Testing Using Spherical Polygons, Graphics Gems V, Academic Press, Inc., 42-49
 
3.
Estellers V., Zosso D., Lai R., Osher S., Thiran J.P., Bresson X., 2012, Efficient algorithm for level set method preserving distance function, IEEE Transactions on Image Processing, 21, 12, 4722-4734.
 
4.
Hu X.Y., Khoo B.C., Adams N.A., Huang F.L., 2006, A conservative interface method for compressible flows, Journal of Computational Physics, 219, 2, 553-578.
 
5.
Iaccarino G., Verzicco R., 2003, Immersed boundary technique for turbulent flow simulations, Applied Mechanics Reviews, 56, 3, 331-347.
 
6.
Ishida T., Takahashi S., Nakahashi K., 2008, Efficient and robust Cartesian mesh generation for building-cube method, Journal of Computational Science and Technology, 2, 4, 435-446.
 
7.
Kawai S., Larsson J., 2012, Wall-modeling in large eddy simulation: Length scales, grid resolution, and accuracy, Physics of Fluids, 24, 1, 1-10.
 
8.
Lahur P.R., Hashimoto A., Murakami K., 2012, Automatic grid generation for dirty STL data using approximate concave feature, 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, January, 1-10.
 
9.
Li J., Wang W., 2017, Fast and robust GPU-based point-in-polyhedron determination, CAD Computer Aided Design, 87, 20-28 publisher = Elsevier Ltd,.
 
10.
Peskin C.S., 1977, Numerical analysis of blood flow in the heart, Journal of Computational Physics, 25, 3, 220-252.
 
11.
Roth S.D., 1982, Ray casting for modeling solids, Computer Graphics and Image Processing, 18, 2, 109-144.
 
12.
Sussman M., Smereka P., Osher S., 1994, A level set approach for computing solutions to incompressible two-phase flow, Journal of Computational Physics, 114, 1, 146-159.
 
13.
Szilvási-Nagy M., Mátyási G., 2003, Analysis of STL files, Mathematical and Computer Modelling, 38, 7-9, 945-960.
 
14.
Takeda Y., Ueno K., Ishikawa T., Takahashi Y., 2020a, Prediction capability of Cartesian cut-cell method with a wall-stress model applied to high Reynolds number flows, Applied Sciences (Switzerland), 10, 15.
 
15.
Takeda Y., Ueno K., Matsuyama S., Tanno H., 2020b, Coupled numerical analysis of three-dimensional unsteady flow with pitching motion of reentry capsule – investigation of the third harmonics of the aerodynamic force, Transactions of the Japan Society for Aeronautical and Space Sciences, 63, 6, 249-256.
 
16.
Uchiyama T., Kohzai M., Miki H., Hirotani T., Sudani N., Shutoku H., 2019, Experimental investigation of a 160% scaled NASA common research model at low speed conditions, AIAA Scitech 2019 Forum, January, 1-21.
 
eISSN:2543-6309
ISSN:1429-2955
Journals System - logo
Scroll to top