[1] 李鹏, 高振勋, 蒋崇文. 重叠网格方法的研究进展[J]. 力学与实践, 2014, 36(5):551-565. LI P, GAO Z X, JIANG C W. The progress of the overlapping grid techniques[J]. Mechanics in Engineering, 2014, 36(5):551-565(in Chinese). [2] SHIH T I P. Overset grids:Fundamentals and practical issues:AIAA-2002-3259[R]. Reston, VA:AIAA, 2002. [3] 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. TIAN S L, WU Y Z, XIA J. Simulation 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). [4] 伍贻兆, 田书玲, 夏健. 基于非结构动网格的非定常流数值模拟方法[J]. 航空学报, 2011, 32(1):15-26. WU Y Z, TIAN S L, XIA J. Unstructured grid methods for unsteady flow simulation[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(1):15-26(in Chinese). [5] MARSTIN C, MCCONNAUGHEY H. Computational problems on composite grids:AIAA-1984-1611[R]. Reston, VA:AIAA, 1984. [6] KANG Z L, YAN C, YU J, et al. A fast and reliable overset unstructured grids approach[J]. Acta Mechanica Sinica, 2013, 29(2):149-157. [7] 黄宇, 阎超, 王文, 等. 混合重叠网格插值方法的改进及应用[J]. 北京航空航天大学学报, 2017, 43(2):285-292. HUANG Y, YAN C, WANG W, et al. An improved interpolation method for hybrid overset grid and its application[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(2):285-292(in Chinese). [8] 周乃春, 李彬, 郑鸣, 等. 带控制率导弹投放数值模拟[J]. 空气动力学学报, 2013, 31(3):107-115. ZHOU N C, LI B, ZHENG M, et al. Missile separation simulation with control laws[J]. Acta Aerodynamica Sinica, 2013, 31(3):107-115(in Chinese). [9] FARRELL P E, PIGGOTT M D, PAIN C C, et al. Conservative interpolation between unstructured meshes via supermesh construction[J]. Computer Methods in Applied Mechanics and Engineering, 2009, 198(33):2632-2642. [10] ZHENG Y, LIOU M S. Progress in the three-dimensional DRAGON grid scheme:AIAA-2001-2540[R]. Reston, VA:AIAA, 2001. [11] XU K, SUN G, CAI J Y. On interface conservative attributions for computations of the complex flows of high-lift system based on chimera tech-nique[C]//Computer and Automation Engineering (ICCAE), 2010 The 2nd International Conference on IEEE. Piscataway, NJ:IEEE Press, 2010:279-283. [12] 张宇飞, 陈海昕, 符松. 基于高阶守恒重映对窗口嵌入技术的改进[J]. 计算物理, 2011, 28(2):167-173. ZHANG Y F, CHEN H X, FU S. Improvement on window embedment technology with high order conservative remapping[J]. Chinese Journal of Computational Physics, 2011, 28(2):167-173(in Chinese). [13] ZHAO X, GUAN H W, YANG Z, et al. An implicit and globally conservative unstructured chimera grid method:AIAA-2011-0777[R]. Reston, VA:AIAA, 2011. [14] FARRELL P E, MADDISON J R. Conservative interpolation between volume meshes by local Galerkin projection[J]. Computer Methods in Applied Mechanics and Engineering, 2011, 200(1):89-100. [15] MENON S, SCHMIDT D P. Conservative interpolation on unstructured polyhedral meshes:An extension of the supermesh approach to cell-centered finite-volume variables[J]. Computer Methods in Applied Mechanics and Engineering, 2011, 200(41):2797-2804. [16] 徐春光, 董海波, 刘君. 基于单元相交的混合网格精确守恒插值方法[J]. 爆炸与冲击, 2016, 36(3):305-312. XU C G, DONG H B, LIU J. An accurate conservative interpolation method for mixed grid based on the intersection of grid cells[J]. Explosion and Shock Waves, 2016, 36(3):305-312(in Chinese). [17] 崔鹏程, 邓有奇, 唐静, 等.基于伴随方程的网格自适应及误差修正技术[J].航空学报, 2016,37(10):2992-3002. CUI P C, DENG Y Q, TANG J, et al. Adjoint-based grid adaptation and error correction[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(10):2992-3002(in Chinese). [18] BLAZEK J. Computational fluid dynamics:principles and applications[M]. 3rd ed. Oxford:Elsevier, 2015:75-120. [19] KIM J S, KWON O J. Improvement on block LU-SGS scheme for unstructured mesh Navier-Stokes computations:AIAA-2002-1061[R]. Reston, VA:AIAA, 2002. [20] SPALART S R. A one-equation turbulence model for aerodynamic flows:AIAA-1992-0439[R]. Reston, VA:AIAA, 1992. [21] ROE P L. Approximate Riemann solvers, parameter vectors, and difference schemes[J]. Journal of Computational Physics, 1981, 43(2):357-372. [22] 李彬, 唐静, 邓有奇, 等. 并行的多重网格方法在离散伴随优化中的应用[J]. 航空学报, 2014, 35(8):2091-2101. LI B, TANG J, DENG Y Q, et al. Application of parallel multigrid algorithm to discrete adjoint optimization[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(8):2091-2101(in Chinese). [23] BEATRICE R, JAY S. Robust and scalable overset grid assembly for partitioned unstructured meshes:AIAA-2013-0797[R]. Reston, VA:AIAA, 2013. [24] THEOHARIS T, IAN P. Two parallel methods for polygon clipping[J]. Computer Graphics Forum, 2010, 8(2):107-114. [25] MARTINEZ F, RUEDA A J, FEITO F R. A new algorithm for computing Boolean operations on polygons[J]. Computers & Geosciences, 2009, 35(6):1177-1185. [26] 唐静, 邓有奇, 马明生, 等. 飞翼气动优化中参数化和网格变形技术研究[J]. 航空学报, 2015, 36(5):1480-1490. TANG J, DENG Y Q, MA M S, et al. Parametrization and grid deformation techniques for fly-wing shape optimization[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(5):1480-1490(in Chinese). [27] ALAUZET F, MEHRENBERGER M. P1-conservative solution interpolation on unstructured triangular meshes[J]. International Journal for Numerical Methods in Engineering, 2010, 84(13):1552-1588. [28] GARIMELLA R, KUCHARIK M, SHASHKOV M. An efficient linearity and bound preserving conservative interpolation (remapping) on polyhedral meshes[J]. Computers & Fluids, 2007, 36(2):224-237. [29] MAYEUR J, DUMONT A, DESTARAC D, et al. RANS simulations on TMR test cases and M6 wing with the ONERA elsA flow solver:AIAA-2015-1745[R]. Reston, VA:AIAA, 2015. [30] DURRANI N, QIN N. Comparison of RANS, DES and DDES results for ONERA M6 wing at transonic flow speed using an in-house parallel code:AIAA-2011-0190[R]. Reston, VA:AIAA, 2011. [31] DA SILVA R G, AZEVEDO J L F, BASSO E. Simulation of ONERA M6 wing flows for assessment of turbulence modeling capabilities:AIAA-2016-0549[R]. Reston, VA:AIAA, 2016. [32] SAXENA S K, NAIR M T. Implementation and testing of Spalart-Allmaras model in a multi-block code:AIAA-2002-0835[R]. Reston, VA:AIAA, 2002. [33] LUO H, BAUM J D, LÖHNER R. A Hermite WENO-based limiter for discontinuous Galerkin method on unstructured grids[J]. Journal of Computational Physics, 2007, 225(1):686-713. [34] HEIM E R. CFD wing/pylon/finned store mutual interference wind tunnel experiment:AEDC-TSR-91-P4[R]. New York:AEDC, 1991. |