VM-LS-DYNA-SOLVE-002

VM-LS-DYNA-SOLVE-002
Steady State Thermal Analysis of 3D Hollow Spheres with Heat Flux Boundary Condition

Overview

Reference: Kreith, F. (1959). Principles of Heat Transfer (2nd ed.). International Textbook Co.
Analysis Type(s): Steady State Thermal
Element Type(s): Solid
Input Files:Link to Input Files Download Page

Test Case

A hollow sphere has an inner surface temperature Ta of 100°C at ra. The material of the hollow spheres is isotropic. A constant heat flux boundary condition of 11.6091 W/m2 is applied on the outer surface rb. Compute the steady state temperature at rc = 3.51419 m.

Figure 17: Problem Sketch

Problem Sketch

Material PropertiesGeometric PropertiesLoading
k = 1 W/(m°C)ra = 2 mTa = 100°C
rb = 5.02839 m q" = 11.6091 W/m2

Analysis Assumptions and Modeling Notes

LS-DYNA Thermal Solver 11 is used. Three hollow spheres in this example are modeled using ELFORM = 1, 4, and 16. The temperature and flux boundary conditions are applied using the keywords *BOUNDARY_TEMPERATURE and *BOUNDARY_FLUX respectively.

The modeling of the sphere is accomplished using one-eighth symmetry. The heat flow is limited to be only in the radial direction.

The rate of heat dissipation can be expressed as:

At steady state, the rate of heat dissipation Q:

Where the thermal resistance Rac can be expressed:

From the above equations, the analytical solution of Tc is obtained as 36.7617oC.

Figure 18: Hollow sphere models with hex, tet4 and tet10 element meshes

Hollow sphere models with hex, tet4 and tet10 element meshes

Figure 19: Fringe plot of temperature oC for each model

Fringe plot of temperature oC for each model

Results Comparison

 TargetLS-DYNAError (%)
Temperature at rc (hex)36.7617 oC37.86613.00%
Temperature at rc (tet4)36.7617 oC37.82002.88%
Temperature at rc (tet10)36.7617 oC36.58960.47%