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Fluid-structure interaction of panel in supersonic fluid passage

Fluid-structure interaction of panel in supersonic fluid passage
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摘要 Fluid-structure interaction of panel in supersonic fluid passage is studied with subcycling and spline interpolation based predict-correct scheme. The passage is formed with two parallel panels, one is rigid and the other is flexible. The interaction between fluid flows and flexible panel is numerically studied, mainly focused on the effect of dynamic pressure and distance between two parallel panels. Subcycling and spline interpolation based predict-correct scheme is utilized to combine the vibration and fluid analysis and to stabilize long-term calculations to get accurate results. It’s demonstrated that the flutter characteristic of flexible panel is more complex with the increase of dynamic pressure and the decrease of distance between two parallel panels. Via analyzing the propagation and reflection of disturbance in passage, it’s determined as a main cause of the variations. Fluid-structure interaction of panel in supersonic fluid passage is studied with subcycling and spline interpolation based predict-correct scheme. The passage is formed with two parallel panels, one is rigid and the other is flexible. The interaction between fluid flows and flexible panel is numerically studied, mainly focused on the effect of dynamic pressure and distance between two parallel panels. Subcycling and spline interpolation based predict-correct scheme is utilized to combine the vibration and fluid analysis and to stabilize long-term calculations to get accurate results. It ' s demonstrated that the flutter characteristic of flexible panel is more complex with the increase of dynamic pressure and the decrease of distance between two parallel panels. Via analyzing the propagation and reflection of disturbance in passage, it' s determined as a main cause of the variations.
出处 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2008年第5期663-668,共6页 哈尔滨工业大学学报(英文版)
关键词 panel flutter fluid-structure interaction subcycling predict-correct scheme 翼段颤振 流体结构 航空科学 气动弹性力学
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  • 1刘占生,张云峰.拉伸弹簧与扭转弹簧模拟动态网格方法分析与改进[J].哈尔滨工业大学学报,2005,37(8):1098-1102. 被引量:10
  • 2CHAKRAVARTHY S R, SZEMA K Y. Computational fluids dynamics capability for internally carried store separation[R]. Rockwell Intl. Corp. Rep. SC-71039-TR, Science Center, Thousands Oaks, CA, 1991. 被引量:1
  • 3FARHAT C, DEGAND C, KOOBUS B, et al. Torsional spring for two-dimensional dynamic unstructured fluid meshes [J]. Computer Methods in Applied Mechanics and Engineering, 1998, 163(1-4): 231-245. 被引量:1
  • 4DEGAND C, FARHAT C. A three-dimensional torsional spring analogy method for unstructured dynamic meshes [J]. Computers and Structures, 2003, 80(3-4): 305-316. 被引量:1
  • 5PRANANTA B B, HOUNJET M H L, ZWAAN R J. Two-dimensional transonic aeroelastic analysis using Thin-Layer Navier-Stokes methods [J]. Journal of Fluids and Structures, 1998, 12(6): 655-676. 被引量:1
  • 6EDWARDS J W, BENNETT R W. WHITLOW Jr W, et al Time marching transonic flutter solutions including angle of attach effects[R]. AIAA Paper 82-0685, AIAA, 1982. 被引量:1
  • 7FARHAT C, LESOINNE C, LETALLEC P. Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: momenrum and energy conservation, optimal discrimination and application to aeroelasticity[J]. Computer Methods in Applied Mechanics and Engineering, 1998, 157(1-2): 95-114. 被引量:1
  • 8PIPERNO S. Partitioned procedures for the transient solution of coupled aeroelastic problems-part Ih Energy transfer analysis and three-dimensional applications[J]. Computer Methods in Applied Mechanics and Engineering, 2001, 190(24-25): 3 147-3 170. 被引量:1
  • 9GORDNIER R E, VISBAL M R. Development of a three-dimensional viscous aeroelastic solver for nonlinear panel flutter[J]. Journal of Fluids and Structures, 2002, 16(4): 497-527. 被引量:1
  • 10HIRT C W, AMSDEN A A, COOK J L. An arbitrary Lagrangian-Eulerian computing method for all flow speeds[J]. Journal of Computational Physics, 1974, 14(3): 227-253. 被引量:1

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