Nonlinear response of thin cylindrical shells with longitudinal cracks and subjected to internal pressure and axial compression loads
- 7 April 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Nonlinear response of damaged stiffened shells subjected to combined internal pressure and mechanical loadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Some computational tools for the analysis of through cracks in stiffened fuselage shellsComputational Mechanics, 1993
- Progress in Collapse AnalysesJournal of Pressure Vessel Technology, 1987
- Some computational aspects of the stability analysis of nonlinear structuresComputer Methods in Applied Mechanics and Engineering, 1984