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Block-Structured AMR for Fluid Structure Interactions

In this study, an immersed boundary (IB) approach on the basis of moving least squares (MLS) interpolation is proposed for analyzing the dynamic response of a rigid body immersed in incompressible flows. An improved mapping strategy is proposed for a quick update of the signed distance field. A CIP–CSL (constraint interpolation profile - semi-Lagrangian) scheme with compact stencils is adopted for the convective part in momentum equation. Fluid-structure interaction problems can be solved by either the weak or the strong coupling schemes according to the density ratio of the solid and fluid. This research is based on our previous research on block-structured adaptive mesh refinement (AMR) method for incompressible flows (Liu and Hu, J. Comput. Phys., 359 (2018), 239-262).

 

Fig. 1 (a) Definition of the non-inertia and inertia reference frame and the Euler angle.

 

Fig. 2 3-D Blocks and its topological structure.

 

Vortex Induced Vibration of a Circular Cylinder

Fig. 3 Time evolution of the drag coefficients () and lift coefficients () for flow over a freely vibrating circular cylinder (, ),: ; ∙∙∙∙∙: .

 

Fig. 4 Vorticity contours of flow past a freely vibrating circular cylinder (, ).

 

(a)  Displacement curves

(b)  , and  curves

 

Fig. 5 Displacement and velocity response for freely vibrating circular cylinder in free-stream () : ;- - -:.

 

Flow past a Rotational Galloping Rectangle

 

Fig. 6 Time evolution of the pitch angle () for rotational galloping square cylinder (, , ,).: Present results; ‑ ‑ ‑: results of Yang and Stern.

 

 

Fig. 7 Vorticity contours in different pitch angle () for flow over rotational galloping square cylinder (, , ,).

 

Freely Falling Rectangular Plate

Fluttering Mode

Fig. 8 Trajectory of the mass center for freely falling plate with fluttering motion. : present simulation, ‑ ‑ ‑: results of experiment.

 

(a),

(c)   ,

 

Fig. 9 Transverse velocity and rotational velocity varying with time,: present simulation, ‑ ‑ ‑: results of experiment.

 

 

Fig. 10 Snapshot of vorticity contours for freely falling rectangular plate with fluttering motion.

 

 

Fig. 11 (a) Blocks and vortex structure for the test of freely falling rectangular plate with fluttering motion ()

 

Tumbling Mode

Fig. 12 Trajectory of the mass center for freely falling plate with tumbling motion. : present simulation, ‑ ‑ ‑: results of experiment.

 

 

Fig. 12 (a) Blocks and vortex structure for the test of freely falling rectangular plate with tumbling motion ().

 

Reference

C. Liu*, C. Hu, Blocked-Based Adaptive Mesh Refinement for Fluid Structure Interactions in Incompressible Flows, submitted.

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