Citation: | XUAN Chuanwei, HAN Jinglong. Explicit assembly algorithm of unstructured overset grid[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(10): 2026-2034. doi: 10.13700/j.bh.1001-5965.2019.0020(in Chinese) |
To solve the problem that the hole mapping method occupies too much physical memory, an improved hole mapping method was developed. Based on the neighbor-to-neighbor search algorithm, a donor search method based on adjacent front was developed. An explicit assembly algorithm of unstructured overset grid was presented by combining the cut-paste method with the implicit cutting technique. First, the algorithm generated a set of Cartesian grids surrounding the wall surface. Second, those Cartesian cells intersecting the wall surface were stored. Finally, relative positions of the stored Cartesian cells were used to determine whether a grid point was inside the wall. After successfully determining all the grid points inside the wall, the current fringe grid points were used as the initial front, and the overlapping area was optimized by the wall distance of each grid point to generate the final interpolation boundary. The proposed explicit algorithm optimizes the traditional implicit assembly process of unstructured overset grid. It features in low physical memory occupation, low cost of donor searching and high computational efficiency. The accuracy and applicability of the proposed explicit method were verified by two typical complex flow examples.
[1] |
BENEK J A, STEGER J L, DOUGHERTY F C.A flexible grid embedding technique with applications to the Euler equations: AIAA-1983-1944[R].Reston, VA: AIAA, 1983.
|
[2] |
NAKAHASHI K, GUMIYA T.An intergrid boundary definition method for overset unstructured grid approach: AIAA-1999-3304[R].Reston, VA: AIAA, 1999.
|
[3] |
TOGASHI F, NAKAHASHI K, ITO Y, et al.Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids: AIAA-2000-1007[R].Reston, VA: AIAA, 2000.
|
[4] |
TOGASHI F, ITO Y, MURAYAMA M, et al.Flow simulation of flapping wings of an insect using overset unstructured grid: AIAA-2001-2619[R].Reston, VA: AIAA, 2001.
|
[5] |
TOGASHI F, ITO Y.Extensions of overset unstructured grids to multiple bodies in contact: AIAA-2002-2809[R].Reston, VA: AIAA, 2002.
|
[6] |
TOGASHI F, ITO Y.Overset unstructured grids method for viscous flow computations: AIAA-2003-3405[R].Reston, VA: AIAA, 2003.
|
[7] |
LEE Y L, BAEDER J D.Implicit hole cutting-a new approach for overset grid connectivity: AIAA-2003-4128[R].Reston, VA: AIAA, 2003.
|
[8] |
XIAO T, QIN N, LUO D, et al.Deformable overset grid for multibody unsteady flow simulation[J].AIAA Journal, 2016, 54(8):2392-2406. doi: 10.2514/1.J054861
|
[9] |
XU X, WANG X D, ZHANG M, et al.A parallelized hybrid N-S/DSMC-IP approach based on adaptive structured/unstructured overlapping grids for hypersonic transitional flows[J].Journal of Computational Physics, 2018, 371(15):409-433. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=1b9221ba7402ff0dd9f9bb4824ca049c
|
[10] |
MISHRA A, BAEDER J D.Coupled aeroelastic prediction of the effects of leading-edge slat on rotor performance[J].Journal of Aircraft, 2012, 53(1):141-157. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=b5217116c6b8d10419560f62f0b8d0f6
|
[11] |
LEE Y, BAEDER J.High-order overset method for blade vortex interaction[C]//AIAA Aerospace Sciences Meeting & Exhibit.Reston, VA: AIAA, 2013: 1-10.
|
[12] |
LOHNER R, SHAROV D, LUO H.Overlapping unstructured grids: AIAA-2001-0439[R].Reston, VA: AIAA, 2001.
|
[13] |
LUO H.An overlapping unstructured grid method for viscous flows: AIAA-2001-2603[R].Reston, VA: AIAA, 2001.
|
[14] |
LANDMANN B, MONTAGNAC M.A highly automated parallel Chimera method for overset grids based on the implicit hole cutting technique[J].International Journal for Numerical Methods in Fluids, 2011, 66(6):778-804. doi: 10.1002/fld.2292
|
[15] |
XU J, CAI J, LIU Q, et al.Flow simulations by enhanced implicit-hole-cutting method on overset grids[J].Journal of Aircraft, 2014, 51(5):1401-1409. doi: 10.2514/1.C032283
|
[16] |
田书玲.基于非结构网格方法的重叠网格算法研究[D].南京: 南京航空航天大学, 2008.
TIAN S L.Investigation of overset unstructured grids algorithm[D].Nanjing: Nanjing University of Aeronautics and Astronautics, 2008(in Chinese).
|
[17] |
CHO K W, KWON J H, LEE S.Development of a fully systemized Chimera methodology for steady/unsteady problems[J].Journal of Aircraft, 1999, 36(6):973-980. doi: 10.2514/2.2538
|
[18] |
WEY T C.Development of a mesh interface generator for overlapped structured grids: AIAA-1994-1924[R].Reston, VA: AIAA, 1994.
|
[19] |
BENEK J A, STEGER J L, DOUGHERTY F A.A flexible grid embedding technique with application to the Euler equations: AIAA-1983-1944[R].Reston, VA: AIAA, 1983.
|
[20] |
LABOZZETTA W F, GATZKE T D.MACGS-towards the complete grid generation system: AIAA-1994-1923[R].Reston, VA: AIAA, 1994.
|
[21] |
CHIU I T, MEAKIN R.On automating domain connectivity for overset grids: AIAA-1995-0854[R].Reston, VA: AIAA, 1995.
|
[22] |
CRABILL J A, WITHERDEN F D, JAMESON A.A parallel direct cut algorithm for high-order overset methods with application to a spinning golf ball[J].Journal of Computational Physics, 2018, 374:692-723. doi: 10.1016/j.jcp.2018.05.036
|
[23] |
MEAKIN R L.Object X-rays for cutting holes in composite overset structured grid: AIAA-2001-2537[R].Reston, VA: AIAA, 2001.
|
[24] |
YANG X, YANG A, SI J.Efficient numerical techniques for simulating a rotorcraft flow field with overlapping grids[J].AIAA Journal, 2015, 53(5):1372-1383. doi: 10.2514/1.J053426
|
[25] |
NINI M, MOTTA V, BINDOLINO G, et al.Three-dimensional simulation of a complete vertical axis wind turbine using overlapping grids[J].Journal of Computational & Applied Mathematics, 2014, 270:78-87. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=565bf6891855d8cda68bf38518de2eb1
|
[26] |
DI Y C, GAO G, XU J L, et al.Time-accurate simulation of the aircraft external store separation[J].Applied Mechanics and Materials, 2013, 444-445:854-859. doi: 10.4028/www.scientific.net/AMM.444-445.854
|
[27] |
ZHAO Y, YU B, YU G.A new two-dimensional hybrid grid generation method based on improved hole cutting[J].International Communications in Heat and Mass Transfer, 2014, 54:103-114. doi: 10.1016/j.icheatmasstransfer.2014.03.015
|
[28] |
淮洋, 郝海兵, 姚冰, 等.一种改进型洞映射法[J].航空计算技术, 2015, 45(2):31-34. doi: 10.3969/j.issn.1671-654X.2015.02.008
HUAI Y, HAO H B, YAO B, et al.An improved method of hole-map[J].Aeronautical Computing Technique, 2015, 45(2):31-34(in Chinese). doi: 10.3969/j.issn.1671-654X.2015.02.008
|
[29] |
袁武, 阎超, 席柯.洞映射方法的研究和改进[J].北京航空航天大学学报, 2012, 38(4):563-568. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=bjhkhtdxxb201204027
YUAN W, YAN C, XI K.Investigation and enhancement of hole mapping method[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(4):563-568(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=bjhkhtdxxb201204027
|
[30] |
王文, 阎超, 袁武, 等.鲁棒的结构网格自动化重叠方法[J].航空学报, 2016, 37(10):2980-2991. http://d.old.wanfangdata.com.cn/Periodical/hkxb201610009
WANG W, YAN C, YUAN W, et al.A robust and automatic structured overlapping grid approach[J].Acta Aeronautica et Astronautica Sinica, 2016, 37(10):2980-2991(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201610009
|
[31] |
BONET J, PERAIRE J.An alternating digital tree(ADT) algorithm for 3D geometric searching and intersection problems[J].International Journal for Numerical Methods in Engineering, 1991, 31:1-17. doi: 10.1002/nme.1620310102
|
[32] |
董国国, 王立强.基于动态结构重叠网格的三维外挂物分离的数值模拟[J].航空兵器, 2011(2):21-25. doi: 10.3969/j.issn.1673-5048.2011.02.005
DONG G G, WANG L Q.Three-dimensional store separation simulation using moving structured overlapping grid technique[J].Aero Weaponry, 2011(2):21-25(in Chinese). doi: 10.3969/j.issn.1673-5048.2011.02.005
|
[33] |
田书玲, 伍贻兆, 夏健.用动态非结构重叠网格法模拟三维多体相对运动绕流[J].航空学报, 2007, 28(1):46-51. doi: 10.3321/j.issn:1000-6893.2007.01.008
TIAN S L, WU Y Z, XIA J.Simnlation of flows past multi-body in relative motion with dynamic unstructured overset grid method[J].Acta Aeronautica et Astronautica Sinica, 2007, 28(1):46-51(in Chinese). doi: 10.3321/j.issn:1000-6893.2007.01.008
|
[34] |
CHIN V D, PETER D W, SPAID F W.Flow field measurements about a multi-element airfoil at high Reynolds numbers: AIAA-1993-3137[R].Reston, VA: AIAA, 1993.
|
[35] |
BIEDRON S, JOHNSON C T, WANG L V.Simulations using a concurrent implicit Navier-Stokes solver: AIAA-1995-223[R].Reston, VA: AIAA, 1995.
|