Publication Date:
2019-06-28
Description:
Package of numerical integration programs static, buckling, vibration, and plastic analysis on thin sheels of revolution. Sheels may be subjected to distributed loads, concentrated line loads, and thermal strain. Outputs include stresses, displacement, plastic strains, and vibration and buckling results. Program aids design of aircraft bodies, spacecraft, submarines, and storage tanks. Written in FORTRAN IV for batch execution, program has been implemented on UNIVAC 1108.
Keywords:
MECHANICS
Type:
MFS-23027
,
NASA Tech Briefs (ISSN 0145-319X); 5; 1; P. 74
Format:
text
Permalink