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.
Shell theory automated for rotational structures
NASA Tech Briefs ; 5 , 1
1980-08-01
Miscellaneous
No indication
English
Automated Shell Theory for Rotating Structures (Astros)
NTIS | 1971
|Automated shell theory for rotating structures (ASTROS)
TIBKAT | 1971
|