Behavior of Cylindrical Shells under the Influence of Moving Loads,
Abstract
The authors discuss a closed cylindrival shell, articulately supported along its edges, which is subjected to the action of static longitudinal forces and pressure that is evenly distributed along its lateral surface. At the initial moment, the shell is struck by a compression wave having a flat front and exponentially changing pressure behind the front. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 07, 1972
- Accession Number
- AD0742709
Entities
People
- A. S. Volmir
- E. D. Skurlatov
- L. N. Dolgikh
- V. R. Solonenko
Organizations
- National Air and Space Intelligence Center