DESIGNING MINIMUM-WEIGHT SHELLS,
Abstract
The condition of yield for the maximum tangential stress and the maximum applied stress can be used for obtaining the lower and upper estimates of the limiting loads on plates and shells. In the present work the condition of yield of the maximum a plied stress is used for obtaining the lower limit in the problem of designing cylindrical shells of minimum weight. The upper limit for the given problem has been obtained.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 08, 1965
- Accession Number
- AD0611533
Entities
People
- F. G. Shamiev
Organizations
- National Air and Space Intelligence Center