Accession Number:

ADA133490

Title:

Composite Laminate Weight Optimization on the HX-20

Descriptive Note:

Final technical rept. for period ending May 1983

Corporate Author:

AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1983-08-01

Pagination or Media Count:

32.0

Abstract:

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.

Subject Categories:

  • Laminates and Composite Materials
  • Computer Programming and Software
  • Computer Hardware
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE