期刊文献+

非结构动网格生成的弹簧-插值联合方法 被引量:20

Spring-interpolation Approach for Generating Unstructured Dynamic Meshes
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摘要 提出了基于弹簧法的两点改进,以解决边界发生大变形时的非结构网格变形问题。为了使边界运动引起的网格变形能更好地由边界传递到内部网格中,提出了一种新的基于Delaunay网格插值的弹簧倔强系数逐层改进方法。为了提高弹簧法的计算效率,引入背景网格和直接插值方法,提出了弹簧-插值法。弹簧-插值法首先生成计算域的背景网格(粗网格),然后由弹簧法求解边界运动引起的背景网格变形,最后利用变形后的背景网格直接插值得到计算网格的变形。算例结果表明:改进后的方法一方面有效地提高了动网格的变形能力和变形后的网格质量;另一方面通过降低弹簧法的求解规模,显著地提高了动网格的变形效率。 The article presents two improvements on the spring analogy for unstructured mesh deformation in engineering applications in which large boundary motions are encountered.A gradually updating scheme which generates gradient spring stiffness by the interpolation method on Delaunay graph is proposed to improve the deformation spread.The spring-interpolation approach is proposed to improve the efficiency of the spring ana-logy.The approach first generates a background mesh (coarse mesh) of the solution domain.Then the defor-mation of the background mesh caused by boundary movements is solved by a spring analogy.Finally,the deformation of the computational mesh is obtained by an interpolation method on the background mesh.Examples demonstrate that the presented method significantly improves the deforming ability of meshes as well as the mesh quality after deformation.Additionally,examples also show that the proposed approach improves the efficiency of mesh deformation effectively by reducing the order of the equations of the spring analogy.
出处 《航空学报》 EI CAS CSCD 北大核心 2010年第7期1389-1395,共7页 Acta Aeronautica et Astronautica Sinica
基金 国家"973"计划(2007CB714603 2010CB832701)
关键词 动网格 网格变形 非结构网格 弹簧法 背景网格 Delaunay网格 dynamic meshes mesh deformation unstructured mesh spring analogy background grid Delaunay graph
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参考文献14

  • 1Blom F J.Considerations on the spring analogy[J].International Journal for Numerical Methods in Fluids,2000,32(6):647-668.
  • 2Murayamaa M,Nakahashi K,Matsushima K.A robust method for unstructured volume/surface mesh movement[J].Transactions of the Japan Society for Aeronautical and Space Sciences,2003,46(152):104-112.
  • 3Zenga D,Ethier C R.A semi-torsional spring analogy model for updating unstructured meshes in 3D moving domains[J].Finite Elements in Analysis and Design,2005,41(11-12):1118-1139.
  • 4Markou G A,Mouroutis Z S.The ortho-semi-torsional (OST) spring analogy method for 3D mesh moving boundary problems[J].Computer methods in Applied Mechanics and Engineering,2007,196(4-6):747-765.
  • 5张军,谭俊杰,褚江,任登凤.一种新的非结构动网格的生成方法[J].南京航空航天大学学报,2007,39(5):633-636. 被引量:10
  • 6Liu X Q,Qin N,Xia H.Fast dynamic grid deformation based on Delaunay graph mapping[J].Journal of Computational Physics,2006,211(2):405-423.
  • 7张来平,段旭鹏,常兴华,王振亚,张涵信.基于Delaunay背景网格插值和局部网格重构的变形体动态混合网格生成技术[J].空气动力学学报,2009,27(1):32-40. 被引量:19
  • 8Zhang L P,Chang X H,Duan X P,et al.A block LU-SGS implicit unsteady incompressible flow solver on hybrid dynamic grids for 2D external bio-fluid simulations[J].Computers & Fluids,2009,38(2):290-308.
  • 9Xiao T H,Ang H S.Combination of mesh deformation and overset grid for simulating unsteadyflow of insect flight[J].Modern Physics Letters B,2009,23(3):525-528.
  • 10Rendall T C S,Allen C B.Efficient mesh motion using radial basis functions with data reduction algorithms[J].Journal of Computational Physics,2009,228(17):6231-6249.

二级参考文献68

  • 1张军,谭俊杰,任登凤.副油箱从机翼分离流场的数值模拟[J].自然科学进展,2006,16(8):1033-1037. 被引量:7
  • 2PERKINS D A, REED J I., HAVENS J E. Morphing wing structures for loitering air vehicles [R]. AIAA 2004-1888.
  • 3RAMRKAHYANI D S, LESIENTURE G A. Aircraft structural morphing using tendon actuated compliant cellular trusses[R]. AIAA 2004-1728.
  • 4SECANELL M, SULEMAN A, GAMBOA P. Design of a morphing airfoil for a light unmanned aerial vehicle using high-fidelity aerodynamic shape optimization[R]. AIAA 2005-1891.
  • 5LIU H, WASSERSUG R J, KAWACHI K A. The three- dimensional hydrodynamics of tadpole locomotion [J]. J. Exp. Biol., 1997, 200: 2807-2819.
  • 6WU J W, SUN M. Unsteady aerodynamics forces of a flapping wing[J]. J. Exp. Biol., 2004(207): 1413- 1427.
  • 7NAKAHASHI K, TOGASHI F. An intergrid-boundary definition method for overset unstructured grid approach[R]. AIAA-99 3304.
  • 8LOHNER R, SHAROY D, LUO H, et al. Overlapping unstructured grids[R]. AIAA-01-0439.
  • 9GRUBE B, CARSTENS V. Computational of unsteady transonic flow in harmonically oscillating turbine cascades taking into account viscous effects[J]. ASME Journal of Turbomachinery, 1998,120 ( 1 ) : 104-111.
  • 10SCHULZE S. Transonic aeroelatic simulation of a flexi ble wing section[A]. AGARD structures and Materials Panel workshop on Numerical Unsteady Aerodynamics and Aeroelastics Simulation[C]. AGARD R-822, Aalborg, Denmark,13-17 October 1997,10;1-10:20.

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