An interactive computer graphics approach to the problem of nesting of plane parts on a raw steel format: (Master's thesis), University of Utah, Salt Lake City, USA (August 1973)
✍ Scribed by F.M. Lillehagen
- Publisher
- Elsevier Science
- Year
- 1974
- Tongue
- English
- Weight
- 97 KB
- Volume
- 6
- Category
- Article
- ISSN
- 0010-4485
No coin nor oath required. For personal study only.
✦ Synopsis
tages over the numerical method in solution stability and speed and accuracy of computation. The program can deal with swelling, thermal and irradiation creep. The calculations that use a schematic fuel pin system are described. Jones, P. A. and Berry, R.L.
74.137 'Vibrational transfer functions for complex structures' NASA Tech. Brief Marshall Space Flight Centre (October 1972) Report MFS-20744 A Fortran 4 program has been written to evaluate the effects of the vibrational multiple frequency forcing functions on equipment support areas and at points of applications of the forcing functions. The forcing functions may be single, multiple frequency, random, or complex periodic. The program can analyse any structure composed of up to 50 substructures with a maximum of 162 degrees of freedom in each substructure.
The basic input to the program is the coupled structure modal properties. To use the response transfer function program, finite element and modal analysis programs must be available.
Lillehagen, F.M.
74.138 'An interactive computer graphics approach to the problem of nesting of plane parts on a raw steel format! (Master's thesis),