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| This program has been developed to facilitate analysis and design of laminated preforms which consist of distinct layers of materials. In general, preforms may be constructed with any combination of continuous fiber, fiber mats, woven fabrics and cores. The program will provide effective laminate properties. Thermal as well as mechanical loadings are included in the point stress calculations. The program applications are highlighted below: 1) Effective laminate properties 2) Laminate stiffness (ABD matrix) 3) Lamina point stress/strain calculations 4) Load conditions: in-plane force and moment resultants including thermal effects |
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This work was conducted in a joint effort between the University of Delaware and Michigan State University under the aegis of the National Science Foundation project Manufacturing Education and Training Program in Composite Materials for the DoD and Durable Goods Industries under the DARPA Supplementary Education Awards.
COPYRIGHT © 1999, THE UNIVERSITY OF DELAWARE ALL RIGHTS RESERVED |
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THE MATERIAL PRESENTED IS DERIVED FROM COMPUTER SOFTWARE DEVELOPED AT THE UNIVERSITY OF DELAWARE AND IS PROVIDED AS IS, WITHOUT REPRESENTATION AS TO ITS FITNESS FOR ANY PURPOSE, AND WITHOUT WARRANTY OF ANY KIND, EITHER EXPRESS OR IMPLIED, INCLUDING WITHOUT LIMITATION THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE. THE UNIVERSITY OF DELAWARE SHALL NOT BE LIABLE FOR ANY DAMAGES, INCLUDING SPECIAL, INDIRECT, INCIDENTAL, OR CONSEQUENTIAL DAMAGES, WITH RESPECT TO ANY CLAIM ARISING OUT OF OR IN CONNECTION WITH THE USE OF THE SOFTWARE, EVEN IF IT HAS BEEN OR IS HEREAFTER ADVISED OF THE POSSIBILITY OF SUCH DAMAGES.
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