Accession Number : ADA117869

Title :   Instructions for TI-59 Combined Card/Module Calculations for In-Plane and Flexural Properties of Symmetric Laminates. Revised.

Descriptive Note : Final technical rept. for period ending May 82,

Corporate Author : AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH

Personal Author(s) : Donaldson,Steven L

PDF Url : ADA117869

Report Date : Jun 1982

Pagination or Media Count : 130

Abstract : This report is an updated and expanded version of AFWAL-TR-81-4116. It contains descriptions and step-by-step instructions for the simple, combined use of magnetic cards with the composite materials module, designed for use in TI-59 programmable calculators. Users do not have to be familiar with TI-59 programming. These programs contain the key calculations of the stiffness and strength of unidirectional and symmetrially laminated composites, including sandwich core laminates. Both in-plane and flexural loadings can be applied, giving in-plane and flexural response. Instant calculations can be made for practical use. With the use of a printer, the results can be immediately and permanently recorded. The equation numbers in this report are from Introduction to Composite Materials by Tsai and Hahn, published by Technomic Publishing Company, Westport, Connecticut, July 1980. (Author)

Descriptors :   *Composite materials, *Laminates, *Flexural properties, *Computations, *Computer programs, Magnetic tape, Cards, Mechanical properties, Stiffness, Strength(Mechanics), Unidirectional, Programmed instruction, Symmetry, Modular construction, Sandwich construction, Calculators, Printers(Data Processing)

Subject Categories : Laminates and Composite Materials
      Computer Programming and Software
      Computer Hardware
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE