Large Deflections of a Rectangular in Layout, Slanting Cylindrical Panel with Motionless Edges,
Abstract
The authors use finite-difference theory to solve a number of geometrically nonlinear problems concerning bending of a slanting cylindrical panel which is under the influcence of transverse loads with boundary conditions of rigid closing and hinged fastening. (Author Modified Abstract)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 12, 1973
- Accession Number
- AD0758052
Entities
People
- M. S. Kornishin
- N. N. Stolyarov
Organizations
- National Air and Space Intelligence Center