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A variational flexible multibody formulation for partitioned fluid-structure interaction: Application to bat-inspired drones and unmanned air-vehicles

机译:用于分配的流体结构相互作用的变形柔性多体配方:应用于蝙蝠风格的无人机和无人驾驶空中车辆

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We present a three-dimensional (3D) partitioned aeroelastic formulation for a flexible multibody system interacting with incompressible turbulent fluid flow. While the incompressible Navier-Stokes system is discretized using a stabilized Petrov-Galerkin procedure, the multibody structural system consists of a generic interaction of multiple components such as rigid body, beams and flexible thin shells along with various types of joints and connections among them. A co-rotational framework is utilized for the category of small strain problems where the displacement of the body is decomposed into a rigid body rotation and a small strain component. This assumption simplifies the structural equations and allows for the incorporation of multiple bodies (rigid as well as flexible) in the system. The displacement and rotation constraints at the joints are imposed by a Lagrange multiplier method. The equilibrium conditions at the fluid- structure interface are satisfied by the transfer of tractions and structural displacements via the radial basis function approach, a scattered data interpolation technique, which is globally conservative. For the coupled stability in low structure-to-fluid mass ratio regimes, a nonlinear iterative force correction scheme is employed in the partitioned staggered predictor-corrector scheme. The convergence and generality of the radial basis function mapping are analyzed by carrying out systematic error analysis of the transfer of fluid traction across the non-matching fluid-structure interface where a third-order of convergence is observed. The proposed aeroelastic framework is then validated by considering a flow across a flexible pitching plate configuration with serration at the trailing edge. Finally, we demonstrate the flow across a flexible flapping wing of a bat modeling the bone fingers as beams and the flexible membrane as thin shells in the multibody system along with the joints. (C) 2020 Elsevier Ltd. All rights reserved.
机译:我们介绍了一种三维(3D)分区的空气弹性配方,用于柔性多体系与不可压缩的湍流流体流动相互作用。虽然不可压缩的Navier-Stokes系统是使用稳定的Petrov-Galerkin程序离散化的,但是多体结构系统包括多个部件的通用相互作用,例如刚体,梁和柔性薄壳,以及它们之间的各种类型的关节和连接。共旋转框架用于小应变问题的类别,其中主体的位移分解成刚体旋转和小应变部件。该假设简化了结构方程,并且允许在系统中加入多个主体(刚性以及柔性)。接头处的位移和旋转约束由拉格朗日乘法器方法施加。通过径向基函数方法的牵引力和结构位移的传递,流体结构界面处的平衡条件,是全球保守的散射数据插值技术。为了在低结构到流体质量比制度中的耦合稳定性,在分区交错的预测器校正器方案中采用非线性迭代力校正方案。通过在观察到三阶收敛的非匹配流体结构界面上进行流体牵引的转移的系统误差分析来分析径向基函数映射的收敛和一般性。然后通过在后缘处的锯齿上考虑穿过柔性俯仰板配置的流动来验证所提出的空气弹性框架。最后,我们展示了蝙蝠柔性张开翼的流动,将骨手指造型为梁和柔性膜,作为多体系统中的薄壳以及关节。 (c)2020 elestvier有限公司保留所有权利。

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