VM246

VM246
Cyclic Analysis of an End-Loaded Hollow Cylindrical Cantilever Beam

Overview

Reference: F. P. Beer, E. R. Johnston, Jr., Mechanics of Materials, McGraw-Hill, Inc., New York, NY, 1981, pg 598.
Analysis Type(s): Static-structural analysis
Element Type(s):
3D 8-Node Structural Solid (SOLID185)
3D 20-Node Structural Solid (SOLID186)
3D 10-Node Tetrahedral Structural Solid (SOLID187)
Input Listing: vm246.dat

Test Case

Figure 417: Hollow Cylindrical Cantilever Beam and Loading

Hollow Cylindrical Cantilever Beam and Loading

Figure 418: Beam Cross-Section

Beam Cross-Section

Determine the maximum deflection of an end-loaded hollow cylindrical beam. The beam is fixed at one end and free on the other. The load consists of a downward force of 5 pounds at the free end.

Material PropertiesGeometric PropertiesLoading
E = 70 x 103 psi
ν = 0.3
Outside Radius (Ro) = 0.5 in
Inside Radius (Ri) = 0.25 in
Length (L) = 10 in
P = 5 lb

Analysis Assumptions and Modeling Notes

From the reference, the maximum deflection (δ) in a cantilever beam with end loading can be found using:

where:

The analysis is accomplished with SOLID185, SOLID186, and SOLID187 element types. For each run, a 30° portion of the beam is modeled, meshed and then expanded using the CYCLIC and /CYCEXPAND commands.

To obtain accurate results, KEYOPT settings were issued for each element type. Enhanced strain formulation (KEYOPT,1,2,2) was used for SOLID185. Full integration (KEYOPT,1,2,1) was used for SOLID186. Pure displacement formulation (KEYOPT,1,6,0) was necessary for SOLID187.

Results Comparison

 TargetMechanical APDLRatio
Deflection (SOLID185)0.51870.52131.005
Deflection (SOLID186)0.51870.52121.005
Deflection (SOLID187)0.51870.52211.007