Composite Laminate Weight Optimization on the HX-20
Final technical rept. for period ending May 1983
AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH
Pagination or Media Count:
An automated method is presented for sizing composite laminate to get minimum total thickness. The method can handle multiple, independent inplane loads, Sizing is based on strength requirements. A listing is presented in BASIC for an Epson HX-20 microcomputer.
- Laminates and Composite Materials
- Computer Programming and Software
- Computer Hardware