DEFINITION OF LOWER CRITICAL LOADS DURING LOCAL LOSS OF STABILITY OF THIN SHELLS,
Abstract
Formulas are derived, which determine lower critical loads for: (a) cylindrical shell under action of axial compression; (b) conical shell, compressed by force along the generatrices; (c) spherical shell and spheroid under action of uniform external pressure; and (d) oblate ellipsoid under internal pressure.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 25, 1964
- Accession Number
- AD0605879
Entities
People
- A. V. Sachenkov
Organizations
- National Air and Space Intelligence Center