Simply Supported Thin Plate Under Periodic Pressure

Calculate the peak UZ displacement and bending stress (SY or SX) at the center of a simply supported square plate of side 10 m and thickness 0.05 m subjected to a periodic pressure load defined with respect to time.

File Name

Open drive letter:\Users\Public\Public Documents\SOLIDWORKS\SOLIDWORKS version\samples\Simulation Examples\Verification\NAFEMS_R0016_Test13P.SLDPRT.

Study Type

Three shell studies are created:

Study Name Study Type
Modal_Damping Linear Dynamics - Transient (modal damping)
Rayleigh_Damping Linear Dynamics - Transient (Rayleigh damping)
Frequency Frequency

Mesh Type

Shell mesh for all three studies. Shell thickness = 0.05 m - Thin shell formulation. Element size is 60 cm.

Material Properties

Linear elastic isotropic. Modulus of elasticity (E) = 2 x 1011 N/m2, Mass density (ρ) = 8000 Kg/m3, Poisson's ratio (ν) = 0.3.

Load

Steady state periodic load F = F0 (sin (ωt) - sin (3 ωt)) over the whole plate where: (a) F0 = 100 N/m2, (b) ω = 2 π f, (c) f = 1.2 Hz, and duration of loading = 15 sec. Horizontal axis is time (sec) and vertical axis is pressure (N/m2).

Dynamic Options

  • Number of mode shapes = 16
  • Solution time = 9.0 sec
  • Time step = 0.002 sec

Damping

  • Modal_damping: 2% of critical damping for all 16 modes
  • Rayleigh_damping: Mass coefficient a0 = 0.299, Stiffness coefficient a1 = 1.339 x 10 -3

Results

The steady-state UZ displacement and bending stress response graphs at the center of the plate are in agreement with the analytical results. The graph depicts the UZ displacement time history at the center of the plate. Horizontal axis is time (sec) and vertical axis is UZ (mm).



  Reference SOLIDWORKS Simulation with Modal _Damping SOLIDWORKS Simulation with Rayleigh_Damping
Peak UZ displacement at center 2.863 mm 2.99 mm 2.99 mm
Peak SY bending stress at center 2.018 N/mm2 1.95 N/mm2 1.95 N/mm2

Reference

NAFEMS, Publication R0016, The International Association for the Engineering Analysis Community, "Selected Benchmarks for Forced Vibration," Test 13P, 1989.