29.11.2012 Views

Oasys LS-DYNA Environment 8.1 VOLUME 3 ... - Oasys Software

Oasys LS-DYNA Environment 8.1 VOLUME 3 ... - Oasys Software

Oasys LS-DYNA Environment 8.1 VOLUME 3 ... - Oasys Software

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

<strong>Oasys</strong> <strong>LS</strong>-<strong>DYNA</strong> <strong>Environment</strong>: User Guide (Version <strong>8.1</strong>)<br />

<strong>LS</strong>-<strong>DYNA</strong> Manual Section: *CONTROL_SHELL<br />

Example of: Hemispherical Load<br />

Example Filenames: hemi_load.key<br />

Description:<br />

A spherical shell is subjected to two outward point loads on the x-axis and two inward point loads<br />

on the y-axis.<br />

Model:<br />

The 1/8 symmetry model of a sphere measures 10 inches in radius with a thickness of 0.04 inches.<br />

The model contains 48 shell elements. A force of one pound is applied in the positive x-direction<br />

to the node on the x-axis. A force of one pound is applied in the negative y-direction to the node<br />

on the y-axis. The calculation terminates at 0.018 seconds.<br />

Input:<br />

The element formulation used is the Hughes-Liu shell. If the Belytschko Tsay shell was used<br />

the Belytschko-Wang-Chiang warpage stiffness option (*CONTROL_SHELL) would also have to<br />

be use. The concentrated loads are applied to two nodes (*DEFINE_CURVE,<br />

*LOAD_NODE_POINT).<br />

Results:<br />

The oscillation of the node on the z-axis shows a regular oscillatory behavior.<br />

Reference:<br />

Belytschko, T., Wang and Chiang.<br />

Page A.67

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!