Intermediate : Vortex excited elastic plate
Fluid velocity fringes
*KEYWORD *TITLE *BOUNDARY_SPC_SET_BIRTH_DEATH *CONTROL_IMPLICIT_DYNAMICS *CONTROL_IMPLICIT_GENERAL *CONTROL_IMPLICIT_SOLUTION *CONTROL_TERMINATION *DATABASE_BINARY_D3PLOT *DATABASE_HISTORY_NODE *DATABASE_NODOUT *DEFINE_CURVE_TITLE *ELEMENT_SHELL *ICFD_BOUNDARY_FREESLIP *ICFD_BOUNDARY_FSI *ICFD_BOUNDARY_NONSLIP *ICFD_BOUNDARY_PRESCRIBED_VEL *ICFD_BOUNDARY_PRESCRIBED_PRE *ICFD_CONTROL_FSI *ICFD_CONTROL_OUTPUT *ICFD_CONTROL_TIME *ICFD_DATABASE_DRAG *ICFD_MAT *ICFD_PART *ICFD_PART_VOL *ICFD_SECTION *INCLUDE *LOAD_SEGMENT_SET *MAT_ELASTIC *MESH_BL *MESH_SIZE *MESH_SURFACE_ELEMENT *MESH_SURFACE_NODE *MESH_VOLUME *NODE *PARAMETER *PART *SECTION_SHELL *SET_SEGMENT *END
$----------------------------------------------------------------------------- $ $ Example provided by Iñaki (LSTC) $ $ E-Mail: info@dynamore.de $ Web: http://www.dynamore.de $ $ Copyright, 2015 DYNAmore GmbH $ Copying for non-commercial usage allowed if $ copy bears this notice completely. $ $X------------------------------------------------------------------------------ $X $X 1. Run file as is. $X Requires LS-DYNA MPP R8.0.0 (or higher) with double precision $X $X------------------------------------------------------------------------------ $# UNITS: (kg/m/s) $X------------------------------------------------------------------------------ $X *KEYWORD *TITLE ICFD Vortex excited elastic plate $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 $ $ $ PARAMETERS $ $ $ $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 *PARAMETER R T_end 15.0 R dt_plot 0.25 R fsi_bt 10. $ $--- Fluid $ R v_inlet 0.315 Rrho_fluid 1.18 R mu_fluid 1.82e-5 R dt_fluid 0.001 *INCLUDE mesh.k *INCLUDE struc.k $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 $ $ $ ICFD CONTROL CARDS $ $ $ $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 *ICFD_CONTROL_TIME $# ttm dt &T_end &dt_fluid *ICFD_CONTROL_FSI $# owc bt 0 &fsi_bt *ICFD_CONTROL_OUTPUT $# mslv 4 $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 $ $ $ ICFD PARTS/ SECTION/ MATERIAL $ $ $ $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 *ICFD_SECTION $# sid 1 *ICFD_MAT $# mid flg ro vis 1 1&rho_fluid &mu_fluid *ICFD_PART $# pid secid mid 1 1 1 *ICFD_PART $# pid secid mid 2 1 1 *ICFD_PART $# pid secid mid 3 1 1 *ICFD_PART $# pid secid mid 4 1 1 *ICFD_PART $# pid secid mid 5 1 1 *ICFD_PART $# pid secid mid 6 1 1 *ICFD_PART_VOL $# pid secid mid 10 1 1 $# spid1 spid2 spid3 spid4 spid5 spid6 1 2 3 4 5 6 $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 $ $ $ ICFD BOUNDARY/INITIAL CONDITIONS $ $ $ $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 *ICFD_BOUNDARY_PRESCRIBED_VEL $# pid dof vad lcid 1 1 1 1 *ICFD_BOUNDARY_PRESCRIBED_VEL $# pid dof vad lcid 1 2 1 2 *ICFD_BOUNDARY_PRESCRIBED_PRE $# pid lcid sf death birth 2 2 *ICFD_BOUNDARY_FREESLIP $# pid 3 *ICFD_BOUNDARY_NONSLIP $# pid 4 *ICFD_BOUNDARY_FSI $# pid 5 *ICFD_BOUNDARY_NONSLIP $# pid 5 *DEFINE_CURVE_TITLE Velocity inlet $# lcid sidr sfa sfo offa offo dattyp 1 $# a1 o1 0.0 &v_inlet 10000.0 &v_inlet *DEFINE_CURVE_TITLE Pressure outlet $# lcid sidr sfa sfo offa offo dattyp 2 $# a1 o1 0.0 0.0 10000.0 0.0 $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 $ $ $ ICFD MESH KEYWORDS $ $ $ $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 *MESH_VOLUME $# volid 10 $# pid1 pid2 pid3 pid4 pid5 1 2 3 4 5 *MESH_BL $# pid nelth 4 1 *MESH_BL $# pid nelth 5 1 *MESH_SIZE $# volid 10 $# pid 6 $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 $ $ $ DATABASE (OUTPUT) $ $ $ $---+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8 *ICFD_DATABASE_DRAG $# pid 4 *ICFD_DATABASE_DRAG $# pid 5 *DATABASE_BINARY_D3PLOT &dt_plot *END
A thin elastic cantilever plate is situated in the wake of a rigid square cylinder. Two configurations are studies. One with no initial deflection, the other with an initial deflection of approx. 2.3cm. In the initial deflection configuration, the beam is released after ten seconds.
References :
[1] W. A. Wall and E. Ramm, “Fluid structure interaction based upon a stabilized (ale) finite element method,” 1998.
[2]B. Hübner, E. Walhorn, and D. Dinkler, “A monolithic approach to fluid–structure interaction using space–time finite elements,” Computer Methods in Applied Mechanics and Engineering, vol. 193, no. 23–26, pp. 2087 – 2104, 2004.
[3] W. A. Wall, Fluid-Struktur-Interaktion mit stabilisierten Finiten Elementen. PhD thesis, Stuttgart University, 1999.