Current Research on Shear Buckling and Thermal Loads with PASCO: Panel Analysis and Sizing Code,
Abstract
A computer program PASCO for obtaining the detailed dimensions optimum (least mass) stiffened composite structural panels is described. Design requirements in terms of inequality constraints can be placed on buckling loads or vibration frequencies lamina stresses and strains, and overall panel stiffness for each of many load conditions. General panel cross sections can be treated.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1981
- Accession Number
- ADP000092
Entities
People
- Melvin S. Anderson
- W. Jefferson Stroud
- William H. Greene
Organizations
- National Aeronautics and Space Administration